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IRIDIUM 136, 42962

Orbit data source: Space-Track

IRIDIUM 136, 42962 is a payload satellite owned by Iridium (US) in LEO that was launched on Mon, 09 Oct 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
42962, 2017-061H
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)
2017-10-09 (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: 22 hours ago

TLE from 22 hours ago
0 IRIDIUM 136
1 42962U 17061H   26316.51164992  .00000072  00000-0  18521-4 0  9993
2 42962  86.3948 323.2801 0002176  89.9153 270.2292 14.34217537476090
Epoch: 2026-11-12T12:16Z
TLE epoch observation values (Epoch: 2026-11-12T12:16:46.553Z)
Latitude
-0.00001°
Longitude
87.44204°
Altitude
780.713 km
Speed
7.463 km/s
True Right ascension
21h 33m 07s
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
06:19:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.189 km
Perigee altitude
773.076 km
Semi-major axis
7,152.769 km
Eccentricity
0.00022
Inclination
86.3948°
RAAN
323.2801°
Arg. of periapsis
89.9153°
True anomaly
270.20427°
Mean anomaly
270.2292°
Eccentric anomaly
270.21673°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000018521
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Documentation

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