Showing default

IRIDIUM 117, 42808

Orbit data source: Space-Track

IRIDIUM 117, 42808 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.

Loading next visibility...
Identifier
42808, 2017-039F
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: 1 day ago

TLE from 1 day ago
0 IRIDIUM 117
1 42808U 17039F   26135.12276584  .00000057  00000-0  13188-4 0  9991
2 42808  86.3993   7.4148 0002298  84.2574 275.8884 14.34217906465236
Epoch: 2026-05-15T02:56Z
TLE epoch observation values (Epoch: 2026-05-15T02:56:46.968Z)
Latitude
-0°
Longitude
90.36049°
Altitude
780.549 km
Speed
7.464 km/s
True Right ascension
00h 29m 39s
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
13:33:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.275 km
Perigee altitude
772.987 km
Semi-major axis
7,152.768 km
Eccentricity
0.00023
Inclination
86.3993°
RAAN
7.4148°
Arg. of periapsis
84.2574°
True anomaly
275.86221°
Mean anomaly
275.8884°
Eccentric anomaly
275.8753°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000013188
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
|