IRIDIUM 119, 42959
Orbit data source: Space-Track
IRIDIUM 119, 42959 is a payload satellite owned by Iridium (US) in LEO that was launched on Mon, 09 Oct 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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42959 intel report (Beta)
IRIDIUM 119 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 119
1 42959U 17061E 24361.42072453 .00000157 00000-0 49110-4 0 9999
2 42959 86.3969 249.9304 0001872 74.3206 285.8196 14.34217712377731
Epoch: 2024-12-26T10:05Z
Definitive object data (Epoch: 2024-12-26T10:05:50.599Z)
Latitude | -0.00004° |
Longitude | 3.0692° |
Altitude | 780.353 km |
Speed | 7.464 km/s |
True Right ascension | 16h 39m 43s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
Latitude | -27.72845° |
Longitude | 0.98062° |
Altitude | 788.365 km |
Speed | 7.458 km/s |
Apparent Right ascension | 13h 30m 56s |
Apparent Declination | -48° 59' 37" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 21:04:25 |
Azimuth | 235.641° WSW |
Elevation | -43.146° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 775.971 km |
Perigee altitude | 773.293 km |
Semi-major axis | 7,152.769 km |
Eccentricity | 0.0001872 |
Inclination | 86.3969° |
RAAN | 249.9304° |
Arg. of periapsis | 74.3206° |
True anomaly | 285.79896° |
Mean anomaly | 285.8196° |
Eccentric anomaly | 285.80928° |
Mean motion | 3.58783 °/min |
BSTAR | 0.00004911 |
Orbital period | 100.34 mins |
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Other satellites on launch #61 in the year 2017 (2017-10-09 UTC)
IRIDIUM 133, 42955 |
IRIDIUM 100, 42956 |
IRIDIUM 122, 42957 |
IRIDIUM 129, 42958 |
IRIDIUM 119, 42959 |
IRIDIUM 107, 42960 |
IRIDIUM 132, 42961 |
IRIDIUM 136, 42962 |
IRIDIUM 139, 42963 |
IRIDIUM 125, 42964 |
IRIDIUM 119 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 05:06:23.526Z | 352.436° N | 2024-12-27 05:10:23.526Z | 227.406° WSW | 43.509° | 2024-12-27 05:14:23.526Z | 185.666° SSW |
6 mins | 2024-12-27 16:23:23.526Z | 117.073° SE | 2024-12-27 16:25:23.526Z | 84.971° E | 22.856° | 2024-12-27 16:29:23.526Z | 30.894° NE |
8 mins | 2024-12-27 18:02:23.526Z | 219.624° SW | 2024-12-27 18:06:23.526Z | 287.279° WNW | 29.5° | 2024-12-27 18:10:23.526Z | 342.197° N |
Authenticating...
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