Showing default

IRIDIUM 123, 42804

Orbit data source: Space-Track

IRIDIUM 123, 42804 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
42804, 2017-039B
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: 10 hours ago

TLE from 10 hours ago
0 IRIDIUM 123
1 42804U 17039B   26308.37702404  .00000060  00000-0  14406-4 0  9999
2 42804  86.3924 295.0403 0002166  91.6665 268.4779 14.34217934490041
Epoch: 2026-11-04T09:02Z
TLE epoch observation values (Epoch: 2026-11-04T09:02:54.877Z)
Latitude
0.00001°
Longitude
115.68543°
Altitude
780.759 km
Speed
7.463 km/s
True Right ascension
19h 40m 09s
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
15:17:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.18 km
Perigee altitude
773.082 km
Semi-major axis
7,152.768 km
Eccentricity
0.00022
Inclination
86.3924°
RAAN
295.0403°
Arg. of periapsis
91.6665°
True anomaly
268.45309°
Mean anomaly
268.4779°
Eccentric anomaly
268.46549°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000014406
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
|