Showing default

IRIDIUM 125, 42964

Orbit data source: Space-Track

IRIDIUM 125, 42964 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.

Loading next visibility...
Identifier
42964, 2017-061K
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: 12 hours ago

TLE from 12 hours ago
0 IRIDIUM 125
1 42964U 17061K   26275.90003163 -.00000020  00000-0 -14132-4 0  9993
2 42964  86.4010 340.3824 0002152  81.9660 278.1780 14.34217361470297
Epoch: 2026-10-02T21:36Z
TLE epoch observation values (Epoch: 2026-10-02T21:36:02.732Z)
Latitude
-0.00004°
Longitude
4.75566°
Altitude
780.501 km
Speed
7.464 km/s
True Right ascension
22h 41m 31s
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
03:26:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.172 km
Perigee altitude
773.094 km
Semi-major axis
7,152.77 km
Eccentricity
0.00022
Inclination
86.401°
RAAN
340.3824°
Arg. of periapsis
81.966°
True anomaly
278.15359°
Mean anomaly
278.178°
Eccentric anomaly
278.16579°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
-0.000014132
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|