IRIDIUM 109, 41919
Orbit data source: Space-Track
IRIDIUM 109, 41919 is a payload satellite owned by Iridium (US) in LEO that was launched on Sat, 14 Jan 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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41919 intel report (Beta)
IRIDIUM 109 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 7 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 7 hours ago
0 IRIDIUM 109
1 41919U 17003C 24361.24363759 -.00000105 00000-0 -44700-4 0 9997
2 41919 86.3969 313.2767 0002212 79.8075 280.3370 14.34216889416098Epoch: 2024-12-26T05:50Z
Definitive object data (Epoch: 2024-12-26T05:50:50.287Z)
| Latitude | -0.00006° |
| Longitude | 130.34134° |
| Altitude | 780.437 km |
| Speed | 7.464 km/s |
| True Right ascension | 20h 53m 06s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 79.05652° |
| Longitude | -68.68419° |
| Altitude | 789.552 km |
| Speed | 7.466 km/s |
| Apparent Right ascension | 01h 26m 55s |
| Apparent Declination | 32° 22' 20" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 12:22:17 |
| Azimuth | 345.833° N |
| Elevation | -16.179° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 776.217 km |
| Perigee altitude | 773.052 km |
| Semi-major axis | 7,152.772 km |
| Eccentricity | 0.0002212 |
| Inclination | 86.3969° |
| RAAN | 313.2767° |
| Arg. of periapsis | 79.8075° |
| True anomaly | 280.31206° |
| Mean anomaly | 280.337° |
| Eccentric anomaly | 280.32453° |
| Mean motion | 3.58783 °/min |
| BSTAR | -0.0000447 |
| Orbital period | 100.34 mins |
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Other satellites on launch #3 in the year 2017 (2017-01-14 UTC)
| IRIDIUM 106, 41917 |
| IRIDIUM 103, 41918 |
| IRIDIUM 109, 41919 |
| IRIDIUM 102, 41920 |
| IRIDIUM 105, 41921 |
| IRIDIUM 104, 41922 |
| IRIDIUM 114, 41923 |
| IRIDIUM 108, 41924 |
| IRIDIUM 112, 41925 |
| IRIDIUM 111, 41926 |
IRIDIUM 109 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 21:01:40.664Z | 153.554° SSE | 2024-12-26 21:06:40.664Z | 71.91° E | 32.787° | 2024-12-26 21:10:40.664Z | 18.879° NNE |
| 6 mins | 2024-12-26 22:44:40.664Z | 247.592° W | 2024-12-26 22:46:40.664Z | 275.988° WNW | 19.878° | 2024-12-26 22:50:40.664Z | 329.383° NNW |
| 9 mins | 2024-12-27 09:12:40.664Z | 356.044° N | 2024-12-27 09:17:40.664Z | 204.631° SW | 44.311° | 2024-12-27 09:21:40.664Z | 181.654° SSW |
Authenticating...
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