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IRIDIUM 126, 42809

Orbit data source: Space-Track

IRIDIUM 126, 42809 is a payload satellite owned by Iridium (US) in LEO that was launched on Sun, 25 Jun 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
42809, 2017-039G
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)
2017-06-25 (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: 8 hours ago

TLE from 8 hours ago
0 IRIDIUM 126
1 42809U 17039G   26127.96197893 -.00000002  00000-0 -78007-5 0  9994
2 42809  86.4000  10.4567 0002167  88.9313 271.2131 14.34217503464184
Epoch: 2026-05-07T23:05Z
TLE epoch observation values (Epoch: 2026-05-07T23:05:14.979Z)
Latitude
-0.00004°
Longitude
158.34369°
Altitude
780.686 km
Speed
7.464 km/s
True Right ascension
00h 41m 49s
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
14:53:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.182 km
Perigee altitude
773.082 km
Semi-major axis
7,152.769 km
Eccentricity
0.00022
Inclination
86.4°
RAAN
10.4567°
Arg. of periapsis
88.9313°
True anomaly
271.18827°
Mean anomaly
271.2131°
Eccentric anomaly
271.20069°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.0000078007
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Documentation

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