IRIDIUM 167, 43931
Orbit data source: Space-Track
IRIDIUM 167, 43931 is a payload satellite owned by Iridium (US) in LEO that was launched on Fri, 11 Jan 2019 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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43931 intel report (Beta)
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IRIDIUM 167 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 14 hours ago |
| Origin | |
| Manufacturer | NGIS 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 14 hours ago
0 IRIDIUM 167
1 43931U 19002K 24296.35500251 .00000697 00000-0 24173-3 0 9998
2 43931 86.3961 245.4654 0002487 81.5119 278.6358 14.34220048302553Epoch: 2024-10-22T08:31Z
Definitive object data (Epoch: 2024-10-22T08:31:12.216Z)
| Latitude | -0.0001° |
| Longitude | 86.39598° |
| Altitude | 780.444 km |
| Speed | 7.464 km/s |
| True Right ascension | 16h 21m 51s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 79.46878° |
| Longitude | 105.85002° |
| Altitude | 789.27 km |
| Speed | 7.467 km/s |
| Apparent Right ascension | 05h 18m 23s |
| Apparent Declination | 39° 27' 27" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 17:24:05 |
| Azimuth | 1.119° NNE |
| Elevation | -10.616° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 776.403 km |
| Perigee | 772.845 km |
| Semi-major axis | 7,152.761 km |
| Eccentricity | 0.0002487 |
| Inclination | 86.3961° |
| RAAN | 245.4654° |
| Arg. of periapsis | 81.5119° |
| True anomaly | 278.60762° |
| Mean anomaly | 278.6358° |
| Eccentric anomaly | 278.62171° |
| Mean motion | 3.58784 °/min |
| BSTAR | 0.00024173 |
| Period | 100.34 mins |
No data available
No data available
Other satellites on launch #2 in the year 2019 (2019-01-11 UTC)
| IRIDIUM 180, 43922 |
| IRIDIUM 176, 43923 |
| IRIDIUM 168, 43924 |
| IRIDIUM 173, 43925 |
| IRIDIUM 169, 43926 |
| IRIDIUM 172, 43927 |
| IRIDIUM 175, 43928 |
| IRIDIUM 171, 43929 |
| IRIDIUM 170, 43930 |
| IRIDIUM 167, 43931 |
IRIDIUM 167 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 | 2024-10-23 08:32:14.067Z | 8.925° NNE | 2024-10-23 08:36:14.067Z | 64.69° ENE | 38.417° | 2024-10-23 08:41:14.067Z | 160.69° S |
| 4 mins | 2024-10-23 10:15:14.067Z | 302.814° NW | 2024-10-23 10:17:14.067Z | 276.081° WNW | 15.586° | 2024-10-23 10:19:14.067Z | 251.153° W |
| 8 mins | 2024-10-23 21:29:14.067Z | 193.596° SSW | 2024-10-23 21:32:14.067Z | 242.204° WSW | 42.528° | 2024-10-23 21:37:14.067Z | 356.677° N |