IRIDIUM 130, 43073
Orbit data source: Space-Track
IRIDIUM 130, 43073 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 23 Dec 2017 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payloads include a variety of satellites, spacecraft, and rockets 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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43073 intel report (Beta)
IRIDIUM 130 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 12 hours ago |
| Origin | |
| 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 | Payload Rocket body Debris |
| Shape & HBR | Trap Box + 2 Pan, 9.4 m |
| Radar Cross Section | 14.423 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 12 hours ago
0 IRIDIUM 130
1 43073U 17083D 24361.05869313 .00000031 00000-0 39995-5 0 9991
2 43073 86.3994 187.1280 0001812 91.7650 268.3753 14.34217848366983Epoch: 2024-12-26T01:24Z
Definitive object data (Epoch: 2024-12-26T01:24:31.086Z)
| Latitude | -0.00006° |
| Longitude | 70.95494° |
| Altitude | 780.755 km |
| Speed | 7.463 km/s |
| True Right ascension | 12h 28m 30s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 82.04818° |
| Longitude | 97.3654° |
| Altitude | 789.982 km |
| Speed | 7.466 km/s |
| Apparent Right ascension | 00h 32m 35s |
| Apparent Declination | 37° 03' 31" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:52:33 |
| Azimuth | 4.087° NNE |
| Elevation | -12.889° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 775.927 km |
| Perigee altitude | 773.335 km |
| Semi-major axis | 7,152.768 km |
| Eccentricity | 0.0001812 |
| Inclination | 86.3994° |
| RAAN | 187.128° |
| Arg. of periapsis | 91.765° |
| True anomaly | 268.35454° |
| Mean anomaly | 268.3753° |
| Eccentric anomaly | 268.36492° |
| Mean motion | 3.58783 °/min |
| BSTAR | 0.0000039995 |
| Orbital period | 100.34 mins |
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Other satellites on launch #83 in the year 2017 (2017-12-23 UTC)
| IRIDIUM 135, 43070 |
| IRIDIUM 138, 43071 |
| IRIDIUM 116, 43072 |
| IRIDIUM 130, 43073 |
| IRIDIUM 151, 43074 |
| IRIDIUM 134, 43075 |
| IRIDIUM 137, 43076 |
| IRIDIUM 141, 43077 |
| IRIDIUM 153, 43078 |
| IRIDIUM 131, 43079 |
IRIDIUM 130 Visibility forecast
Observer location: undefined°, undefined
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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2024-12-26 23:45:52.340Z | 31.827° NE | 2024-12-26 23:48:52.340Z | 72.186° E | 21.408° | 2024-12-26 23:52:52.340Z | 127.148° SE |
| 7 mins | 2024-12-27 01:26:52.340Z | 331.109° NNW | 2024-12-27 01:29:52.340Z | 278.688° WNW | 31.379° | 2024-12-27 01:33:52.340Z | 212.981° SW |
| 8 mins | 2024-12-27 12:41:52.340Z | 155.117° SSE | 2024-12-27 12:45:52.340Z | 71.551° E | 36.574° | 2024-12-27 12:49:52.340Z | 15.792° NNE |
Authenticating...
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