IRIDIUM 124, 42810
Orbit data source: Space-Track
IRIDIUM 124, 42810 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.
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42810 intel report (Beta)
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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, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 IRIDIUM 124
1 42810U 17039H 26307.54603557 .00000128 00000-0 32194-4 0 9992
2 42810 86.4509 232.0671 0002107 84.4341 275.7100 14.43281039495212Epoch: 2026-11-03T13:06Z
TLE epoch observation values (Epoch: 2026-11-03T13:06:17.473Z)
Latitude
-0.00003°
Longitude
-7.31286°
Altitude
750.594 km
Speed
7.479 km/s
True Right ascension
15h 28m 16s
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
04:17:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
746.13 km
Perigee altitude
743.128 km
Semi-major axis
7,122.766 km
Eccentricity
0.00021
Inclination
86.4509°
RAAN
232.0671°
Arg. of periapsis
84.4341°
True anomaly
275.68597°
Mean anomaly
275.71°
Eccentric anomaly
275.69799°
Mean motion
3.61052 °/min
Orbital period
99.71 mins
BSTAR
0.000032194
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Other satellites on launch #39 in the year 2017 (2017-06-25 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.IRIDIUM 124 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-11-04 19:09:41.181Z | 159.451° S | 2026-11-04 19:14:41.181Z | 76.15° E | 46.726° | 2026-11-04 19:18:41.181Z | 16.473° NNE |
| 5 mins | 2026-11-04 20:52:41.181Z | 254.969° W | 2026-11-04 20:54:41.181Z | 282.881° WNW | 17.956° | 2026-11-04 20:57:41.181Z | 322.078° NNW |
| 8 mins | 2026-11-05 07:17:41.181Z | 353.989° N | 2026-11-05 07:20:41.181Z | 318.197° NNW | 75.844° | 2026-11-05 07:25:41.181Z | 183.231° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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