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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 (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: 13 hours ago

TLE from 13 hours ago
0 IRIDIUM 129
1 42958U 17061D   26275.88100432  .00000019  00000-0 -10836-6 0  9996
2 42958  86.4006 340.2596 0002294  94.3222 265.8236 14.34217610470239
Epoch: 2026-10-02T21:08Z
TLE epoch observation values (Epoch: 2026-10-02T21:08:38.773Z)
Latitude
-0.00001°
Longitude
11.50145°
Altitude
780.839 km
Speed
7.463 km/s
True Right ascension
22h 41m 02s
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
03:27:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.273 km
Perigee altitude
772.991 km
Semi-major axis
7,152.769 km
Eccentricity
0.00023
Inclination
86.4006°
RAAN
340.2596°
Arg. of periapsis
94.3222°
True anomaly
265.79738°
Mean anomaly
265.8236°
Eccentric anomaly
265.81049°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-1.0836e-7
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