IRIDIUM 115, 42806
Orbit data source: Space-Track
IRIDIUM 115, 42806 is a payload satellite owned by Iridium (US) in LEO that was launched on Sun, 25 Jun 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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42806 intel report (Beta)
IRIDIUM 115 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 115
1 42806U 17039D 24361.45791466 .00000370 00000-0 10404-3 0 9990
2 42806 86.4519 186.7802 0001597 83.9204 276.2179 14.43282819396706Epoch: 2024-12-26T10:59Z
Definitive object data (Epoch: 2024-12-26T10:59:23.826Z)
| Latitude | -0.00002° |
| Longitude | -73.5061° |
| Altitude | 750.614 km |
| Speed | 7.479 km/s |
| True Right ascension | 12h 27m 07s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 83.00117° |
| Longitude | -43.47092° |
| Altitude | 760.199 km |
| Speed | 7.482 km/s |
| Apparent Right ascension | 05h 56m 51s |
| Apparent Declination | 34° 43' 45" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 17:24:24 |
| Azimuth | 353.106° N |
| Elevation | -14.98° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 745.761 km |
| Perigee altitude | 743.486 km |
| Semi-major axis | 7,122.76 km |
| Eccentricity | 0.0001597 |
| Inclination | 86.4519° |
| RAAN | 186.7802° |
| Arg. of periapsis | 83.9204° |
| True anomaly | 276.19971° |
| Mean anomaly | 276.2179° |
| Eccentric anomaly | 276.2088° |
| Mean motion | 3.61053 °/min |
| BSTAR | 0.00010404 |
| Orbital period | 99.71 mins |
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Other satellites on launch #39 in the year 2017 (2017-06-25 UTC)
| IRIDIUM 113, 42803 |
| IRIDIUM 123, 42804 |
| IRIDIUM 120, 42805 |
| IRIDIUM 115, 42806 |
| IRIDIUM 118, 42807 |
| IRIDIUM 117, 42808 |
| IRIDIUM 126, 42809 |
| IRIDIUM 124, 42810 |
| IRIDIUM 128, 42811 |
| IRIDIUM 121, 42812 |
IRIDIUM 115 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 | 2024-12-27 00:52:58.714Z | 354.02° N | 2024-12-27 00:56:58.714Z | 251.543° W | 44.402° | 2024-12-27 01:00:58.714Z | 184.473° SSW |
| 5 mins | 2024-12-27 12:05:58.714Z | 114.906° SE | 2024-12-27 12:07:58.714Z | 85.23° E | 19.898° | 2024-12-27 12:10:58.714Z | 41.767° NE |
| 7 mins | 2024-12-27 13:44:58.714Z | 219.486° SW | 2024-12-27 13:47:58.714Z | 277.134° WNW | 32.108° | 2024-12-27 13:51:58.714Z | 342.732° N |
Authenticating...
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