LEMUR 2 PETERG, 42841
Orbit data source: Space-Track
LEMUR 2 PETERG, 42841 is a payload satellite owned by Spire (US) in SSO that was launched on Fri, 14 Jul 2017 UTC via a SOYUZ-2-1A launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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42841 intel report (Beta)
LEMUR 2 PETERG details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 13 hours ago |
| Origin | |
| Manufacturer | Spire/Glasgow |
| Mission | Operational Commercial Com/MetRO |
| Bus & Motor | CUBESAT 3U, Unknown motor |
| Mass | 4 kg wet, 4 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box, 0.5 m |
| Radar Cross Section | 0.093 m², Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 13 hours ago
0 LEMUR 2 PETERG
1 42841U 17042S 24361.51870007 .00023070 00000-0 13580-2 0 9998
2 42841 97.3881 184.2343 0006665 74.0197 286.1768 15.11610691406631Epoch: 2024-12-26T12:26Z
Definitive object data (Epoch: 2024-12-26T12:26:55.686Z)
| Latitude | 0.00006° |
| Longitude | -97.99467° |
| Altitude | 533.086 km |
| Speed | 7.597 km/s |
| True Right ascension | 12h 16m 56s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 16.56187° |
| Longitude | 84.74406° |
| Altitude | 533.731 km |
| Speed | 7.597 km/s |
| Apparent Right ascension | 22h 30m 54s |
| Apparent Declination | -45° 05' 17" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 01:16:23 |
| Azimuth | 207.852° SW |
| Elevation | -2.755° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 532.867 km |
| Perigee altitude | 523.661 km |
| Semi-major axis | 6,906.401 km |
| Eccentricity | 0.0006665 |
| Inclination | 97.3881° |
| RAAN | 184.2343° |
| Arg. of periapsis | 74.0197° |
| True anomaly | 286.10343° |
| Mean anomaly | 286.1768° |
| Eccentric anomaly | 286.14012° |
| Mean motion | 3.78151 °/min |
| BSTAR | 0.001358 |
| Orbital period | 95.2 mins |
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Other satellites on launch #42 in the year 2017 (2017-07-14 UTC)
LEMUR 2 PETERG 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2024-12-27 12:23:40.065Z | 164.21° S | 2024-12-27 12:27:40.065Z | 18.724° NNE | 44.108° | 2024-12-27 12:30:40.065Z | 350.236° N |
| 6 mins | 2024-12-28 01:33:40.065Z | 356.439° N | 2024-12-28 01:35:40.065Z | 309.821° NW | 38.452° | 2024-12-28 01:39:40.065Z | 207.459° SW |
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