IRIDIUM 157, 43251
Orbit data source: Space-Track
IRIDIUM 157, 43251 is a payload satellite owned by Iridium (US) in LEO that was launched on Fri, 30 Mar 2018 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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43251 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: 2 days ago
TLE from 2 days ago
0 IRIDIUM 157
1 43251U 18030C 26171.39554921 .00000069 00000-0 17534-4 0 9991
2 43251 86.3962 289.0785 0002210 94.1526 265.9923 14.34217878430594Epoch: 2026-06-20T09:29Z
TLE epoch observation values (Epoch: 2026-06-20T09:29:35.451Z)
Latitude
0.00002°
Longitude
-121.92999°
Altitude
780.829 km
Speed
7.463 km/s
True Right ascension
19h 16m 18s
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
21:47:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.212 km
Perigee altitude
773.05 km
Semi-major axis
7,152.768 km
Eccentricity
0.00022
Inclination
86.3962°
RAAN
289.0785°
Arg. of periapsis
94.1526°
True anomaly
265.96704°
Mean anomaly
265.9923°
Eccentric anomaly
265.97967°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.000017534
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Other satellites on launch #30 in the year 2018 (2018-03-30 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 157 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-22 18:59:52.032Z | 21.336° NNE | 2026-06-22 19:03:52.032Z | 73.245° E | 25.277° | 2026-06-22 19:07:52.032Z | 133.603° SE |
| 7 mins | 2026-06-22 20:41:52.032Z | 325.18° NNW | 2026-06-22 20:44:52.032Z | 275.603° WNW | 26.995° | 2026-06-22 20:48:52.032Z | 218.759° SW |
| 8 mins | 2026-06-23 07:56:52.032Z | 163.278° S | 2026-06-23 07:59:52.032Z | 114.317° SE | 40.466° | 2026-06-23 08:04:52.032Z | 10.98° NNE |
| 4 mins | 2026-06-23 09:39:52.032Z | 265.335° W | 2026-06-23 09:41:52.032Z | 290.861° WNW | 14.112° | 2026-06-23 09:43:52.032Z | 314.759° NW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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