IRIDIUM 100, 42956
Orbit data source: Space-Track
IRIDIUM 100, 42956 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.
Focus sentinelFocus sentinel
Embed this page
Focus sentinelFocus sentinel
42956 intel report (Beta)
Focus sentinelFocus sentinel
Create New Watchlist
Focus sentinelFocus sentinel
Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
OATK SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Trap Box + 2 Pan, 4.7 m
Radar Cross Section
14.423 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 IRIDIUM 100
1 42956U 17061B 25261.06753096 .00000070 00000-0 17988-4 0 9997
2 42956 86.3994 138.9711 0002298 87.4155 272.7304 14.34218185415774Epoch: 2025-09-18T01:37Z
TLE epoch observation values (Epoch: 2025-09-18T01:37:14.674Z)
Latitude
-0.00003°
Longitude
117.42551°
Altitude
780.639 km
Speed
7.464 km/s
True Right ascension
09h 15m 53s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
05:16:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.274 km
Perigee altitude
772.986 km
Semi-major axis
7,152.767 km
Eccentricity
0.00023
Inclination
86.3994°
RAAN
138.9711°
Arg. of periapsis
87.4155°
True anomaly
272.7041°
Mean anomaly
272.7304°
Eccentric anomaly
272.71725°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000017988
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...
Other satellites on launch #61 in the year 2017 (2017-10-09 UTC)
Did you know?
You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IRIDIUM 100 Visibility forecast
Loading observer location...
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-18 15:10:47.546Z | 99.254° ESE | 2025-09-18 15:12:47.546Z | 74.373° E | 13.702° | 2025-09-18 15:14:47.546Z | 50.67° ENE |
| 8 mins | 2025-09-18 16:48:47.546Z | 196.666° SSW | 2025-09-18 16:52:47.546Z | 285.149° WNW | 41.463° | 2025-09-18 16:56:47.546Z | 353.201° N |
| 7 mins | 2025-09-19 03:19:47.546Z | 27.221° NE | 2025-09-19 03:22:47.546Z | 75.298° E | 28.075° | 2025-09-19 03:26:47.546Z | 138.647° SSE |
| 7 mins | 2025-09-19 05:00:47.546Z | 321.05° NNW | 2025-09-19 05:03:47.546Z | 273.198° WNW | 24.234° | 2025-09-19 05:07:47.546Z | 221.724° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
|---|
CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
Authenticating...
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
|---|