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IRIDIUM 102, 41920

Orbit data source: Space-Track

IRIDIUM 102, 41920 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 14 Jan 2017 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
41920, 2017-003D
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
OATK SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
2017-01-14 (9 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Trap Box + 2 Pan, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago
0 IRIDIUM 102
1 41920U 17003D   26138.33604111  .00000170  00000-0  53651-4 0  9998
2 41920  86.3943 100.9185 0002246  86.4454 273.6998 14.34219414489008
Epoch: 2026-05-18T08:03Z
TLE epoch observation values (Epoch: 2026-05-18T08:03:53.951Z)
Latitude
-0.00011°
Longitude
103.91793°
Altitude
780.609 km
Speed
7.464 km/s
True Right ascension
06h 43m 40s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
04:38:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.233 km
Perigee altitude
773.02 km
Semi-major axis
7,152.763 km
Eccentricity
0.00022
Inclination
86.3943°
RAAN
100.9185°
Arg. of periapsis
86.4454°
True anomaly
273.67412°
Mean anomaly
273.6998°
Eccentric anomaly
273.68696°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000053651
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