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IRIDIUM 129, 42958

Orbit data source: Space-Track

IRIDIUM 129, 42958 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
42958, 2017-061D
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 (8 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: 8 hours ago

TLE from 8 hours ago
0 IRIDIUM 129
1 42958U 17061D   25356.85336730  .00000115  00000-0  34075-4 0  9999
2 42958  86.3975  98.9940 0001726  93.8640 266.2753 14.34216654429522
Epoch: 2025-12-22T20:28Z
TLE epoch observation values (Epoch: 2025-12-22T20:28:50.934Z)
Latitude
-0.00005°
Longitude
60.13627°
Altitude
780.802 km
Speed
7.463 km/s
True Right ascension
06h 35m 58s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
03:25:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
775.87 km
Perigee altitude
773.401 km
Semi-major axis
7,152.772 km
Eccentricity
0.00017
Inclination
86.3975°
RAAN
98.994°
Arg. of periapsis
93.864°
True anomaly
266.25556°
Mean anomaly
266.2753°
Eccentric anomaly
266.26543°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000034075
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