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 | 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 141
1 43077U 17083H 24339.86809784 .00000674 00000-0 23350-3 0 9994
2 43077 86.3999 195.7419 0002286 81.3290 278.8165 14.34216213364001Epoch: 2024-12-04T20:50Z
Definitive object data (Epoch: 2024-12-04T20:50:03.653Z)
| Latitude | 0.00001° |
| Longitude | 169.0696° |
| Altitude | 780.473 km |
| Speed | 7.464 km/s |
| True Right ascension | 13h 02m 58s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 52.97849° |
| Longitude | -15.90471° |
| Altitude | 785.295 km |
| Speed | 7.467 km/s |
| Apparent Right ascension | 21h 42m 03s |
| Apparent Declination | 13° 19' 40" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 07:06:53 |
| Azimuth | 317.421° NNW |
| Elevation | -25.708° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 776.272 km |
| Perigee altitude | 773.002 km |
| Semi-major axis | 7,152.774 km |
| Eccentricity | 0.0002286 |
| Inclination | 86.3999° |
| RAAN | 195.7419° |
| Arg. of periapsis | 81.329° |
| True anomaly | 278.79061° |
| Mean anomaly | 278.8165° |
| Eccentric anomaly | 278.80356° |
| Mean motion | 3.58783 °/min |
| BSTAR | 0.0002335 |
| 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2024-12-05 15:22:42.980Z | 192.716° SSW | 2024-12-05 15:26:42.980Z | 303.329° NW | 42.646° | 2024-12-05 15:30:42.980Z | 356.227° N |
| 7 mins | 2024-12-06 01:53:42.980Z | 31.233° NE | 2024-12-06 01:56:42.980Z | 79.596° E | 26.022° | 2024-12-06 02:00:42.980Z | 136.787° SSE |
| 7 mins | 2024-12-06 03:34:42.980Z | 321.362° NNW | 2024-12-06 03:37:42.980Z | 268.998° W | 26.198° | 2024-12-06 03:41:42.980Z | 217.702° SW |
Authenticating...
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