IRIDIUM 141, 43077
Orbit data source: Space-Track
IRIDIUM 141, 43077 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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43077 intel report (Beta)
IRIDIUM 141 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 11 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 11 hours ago
0 IRIDIUM 141
1 43077U 17083H 24361.07772059 .00000073 00000-0 18988-4 0 9991
2 43077 86.3986 186.8870 0001942 80.5384 279.6032 14.34217864367044Epoch: 2024-12-26T01:51Z
Definitive object data (Epoch: 2024-12-26T01:51:55.058Z)
| Latitude | 0.00002° |
| Longitude | 63.8453° |
| Altitude | 780.486 km |
| Speed | 7.464 km/s |
| True Right ascension | 12h 27m 32s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -69.44362° |
| Longitude | 54.03671° |
| Altitude | 804.947 km |
| Speed | 7.449 km/s |
| Apparent Right ascension | 01h 27m 17s |
| Apparent Declination | -77° 00' 19" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:37:22 |
| Azimuth | 184.58° SSW |
| Elevation | -52.526° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 776.02 km |
| Perigee altitude | 773.242 km |
| Semi-major axis | 7,152.768 km |
| Eccentricity | 0.0001942 |
| Inclination | 86.3986° |
| RAAN | 186.887° |
| Arg. of periapsis | 80.5384° |
| True anomaly | 279.58126° |
| Mean anomaly | 279.6032° |
| Eccentric anomaly | 279.59223° |
| Mean motion | 3.58783 °/min |
| BSTAR | 0.000018988 |
| 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 141 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2024-12-26 13:41:43.657Z | 203.683° SW | 2024-12-26 13:46:43.657Z | 287.328° WNW | 35.832° | 2024-12-26 13:50:43.657Z | 347.518° N |
| 8 mins | 2024-12-27 00:13:43.657Z | 21.834° NNE | 2024-12-27 00:16:43.657Z | 78.4° E | 34.044° | 2024-12-27 00:21:43.657Z | 153.938° SSE |
| 6 mins | 2024-12-27 01:54:43.657Z | 314.385° NW | 2024-12-27 01:57:43.657Z | 271.381° WNW | 19.12° | 2024-12-27 02:00:43.657Z | 234.676° WSW |
| 7 mins | 2024-12-27 13:08:43.657Z | 182.179° SSW | 2024-12-27 13:12:43.657Z | 211.506° SW | 44.907° | 2024-12-27 13:15:43.657Z | 0.951° NNE |
Authenticating...
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