INMARSAT 5-F2

40384
Nummer im Katalog Spacetrack
2015-02-01
In die Umlaufbahn bringen
35786.46 km
Höhe Durchschnitt
11068.93 km/h
Durchschnittsgeschwindigkeit

Informationen über den Satelliten. INMARSAT 5-F2

Name im Katalog Spacetrack INMARSAT 5-F2
Folge INMARSAT 5-F2 INMARSAT 5-F2 Tracker
Flugzeiten INMARSAT 5-F2 Flugzeiten INMARSAT 5-F2
In die Umlaufbahn bringen 2015-02-01 (10 vor Jahren)
Tage im Orbit 3789
Herkunftsland/-organisation International Mobile Satellite Organization (INMARSAT) (IM)
Wir analysieren den polnischen Text, der 'Miejsce startu' lautet. TYMSC (Baikonur Cosmodrome, Kazakhstan)
Kategorie
Perygeum 35784 km
Apogäum 35788 km
Neigung der Umlaufbahn (Inklination) 0.01°
Runden pro Tag 1
Orbit GEO
Höhe INMARSAT 5-F2 35786.46 km

Informationen über INMARSAT 5-F2

An emergency position-indicating radiobeacon (EPIRB) is a type of emergency locator beacon, a portable battery powered radio transmitter used in emergencies to locate airplanes, vessels, and persons in distress and in need of immediate rescue. In the event of an emergency, such as the ship sinking or an airplane crash, the transmitter is activated and begins transmitting a continuous radio signal which is used by search and rescue teams to quickly locate the emergency and render aid. The signal is detected by satellites operated by an international consortium of rescue services, COSPAS-SARSAT. The basic purpose of this system is to help rescuers find survivors within the so-called "golden day" (the first 24 hours following a traumatic event) during which the majority of survivors can usually be saved. The feature distinguishing modern EPIRBs, often called GPIRBs, from other types of emergency beacon is that it contains a GPS receiver and broadcasts its position, usually accurate within 100 meters, to facilitate location.
The standard frequency of a modern EPIRB is 406 MHz. It is an internationally-regulated mobile radiocommunication service that aids search and rescue operations to detect and locate distressed boats, aircraft, and people. It is distinct from a Satellite emergency position-indicating radiobeacon station.
The first form of these beacons was the 121.500 MHz ELT, which was designed as an automatic locator beacon for crashed military aircraft. These beacons were first used in the 1950s by the U.S. military and were mandated for use on many types of commercial and general aviation aircraft beginning in the early 1970s. The frequency and signal format used by the ELT beacons was not designed for satellite detection, which resulted in a system with poor location detection abilities and with long delays in detection of activated beacons. The satellite detection network was built after the ELT beacons were already in general use, with the first satellite not being launched until 1982, and even then, the satellites only provided detection, with location accuracy being roughly 20 km. The technology was later expanded to cover use on vessels at sea (EPIRB), individual persons (PLB and, starting in 2016, MSLD). All have migrated from using 121.500 MHz as their primary frequency to using 406 MHz, which was designed for satellite detection and location.Since the inception of Cospas-Sarsat in 1982, distress radiobeacons have assisted in the rescue of over 28,000 people in more than 7,000 distress situations. In 2010 alone, the system provided information used to rescue 2,388 persons in 641 distress situations.

der Satellit INMARSAT 5-F2 hinausgetragen 01.02.2015r. Durchschnittshöhe INMARSAT 5-F2 Text Nummer 1: das. 35786.46 km. Durchschnittsgeschwindigkeit INMARSAT 5-F2 beträgt 11068.93 km/h. Neigung INMARSAT 5-F2 Satelliten 0.02°.

Orbital Elemente

Zeige formatiertes JSON.

Durchschnittshöhe der Orbitalbahn. INMARSAT 5-F2

Durchschnittsgeschwindigkeit INMARSAT 5-F2

Durchschnitt INMARSAT 5-F2

Aktualisierungsdatum.: 2025-06-17 07:30:13
Durchschnittshöhe INMARSAT 5-F2 beträgt: 35786.46km
Durchschnittsgeschwindigkeit INMARSAT 5-F2 beträgt: 11068.93km/h
Durchschnittliche Neigung der Bahn INMARSAT 5-F2 beträgt: 0.02°
INMARSAT 5-F2 wurde am Tag in eine Umlaufbahn gebracht 2015-02-01
INMARSAT 5-F2 ist von 3789 Tage in der Umlaufbahn.