Showing default

IRIDIUM 139, 42963

Orbit data source: Space-Track

IRIDIUM 139, 42963 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
42963, 2017-061J
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: 13 hours ago

TLE from 13 hours ago
0 IRIDIUM 139
1 42963U 17061J   26095.97970342  .00000337  00000-0  11333-3 0  9999
2 42963  86.3961  55.4918 0002309  88.9702 271.1759 14.34214997444490
Epoch: 2026-04-05T23:30Z
TLE epoch observation values (Epoch: 2026-04-05T23:30:46.375Z)
Latitude
0.00004°
Longitude
-131.47878°
Altitude
780.694 km
Speed
7.464 km/s
True Right ascension
03h 41m 58s
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
18:06:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.292 km
Perigee altitude
772.989 km
Semi-major axis
7,152.778 km
Eccentricity
0.00023
Inclination
86.3961°
RAAN
55.4918°
Arg. of periapsis
88.9702°
True anomaly
271.14945°
Mean anomaly
271.1759°
Eccentric anomaly
271.16267°
Mean motion
3.58782 °/min
Orbital period
100.34 mins
BSTAR
0.00011333
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
|