LEMUR 2 THENICKMOLO, 43185
Orbit data source: Space-Track
LEMUR 2 THENICKMOLO, 43185 is a payload satellite owned by Spire (US) in SSO that was launched on Thu, 01 Feb 2018 UTC via a SOYUZ-2-1A launch vehicle from the Vostochny Cosmodrome (VOSTO). 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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43185 intel report (Beta)
LEMUR 2 THENICKMOLO details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 8 hours ago |
| Origin | |
| Manufacturer | Spire/Glasgow |
| Mission | Operational Commercial Com/MetRO |
| Bus & Motor | CUBESAT 3U, Unknown motor |
| Mass | 4.6 kg wet, 4.6 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, 0.7 m |
| Radar Cross Section | 0.124 m², Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 8 hours ago
0 LEMUR 2 THENICKMOLO
1 43185U 18014F 24361.28932534 .00050816 00000-0 17023-2 0 9992
2 43185 97.5732 266.3180 0008201 37.4329 322.7481 15.30730795378017Epoch: 2024-12-26T06:56Z
Definitive object data (Epoch: 2024-12-26T06:56:37.709Z)
| Latitude | -0.00004° |
| Longitude | 66.89003° |
| Altitude | 472.259 km |
| Speed | 7.632 km/s |
| True Right ascension | 17h 45m 16s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 1.00784° |
| Longitude | 67.09042° |
| Altitude | 471.907 km |
| Speed | 7.633 km/s |
| Apparent Right ascension | 20h 45m 48s |
| Apparent Declination | -35° 05' 51" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 14:09:27 |
| Azimuth | 113.904° SE |
| Elevation | -27.908° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 476.206 km |
| Perigee altitude | 464.973 km |
| Semi-major axis | 6,848.726 km |
| Eccentricity | 0.0008201 |
| Inclination | 97.5732° |
| RAAN | 266.318° |
| Arg. of periapsis | 37.4329° |
| True anomaly | 322.69117° |
| Mean anomaly | 322.7481° |
| Eccentric anomaly | 322.71964° |
| Mean motion | 3.82938 °/min |
| BSTAR | 0.0017023 |
| Orbital period | 94.01 mins |
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Other satellites on launch #14 in the year 2018 (2018-02-01 UTC)
| KANOPUS-V 3, 43180 |
| KANOPUS-V 4, 43181 |
| LEMUR 2 JIN-LUEN, 43182 |
| LEMUR 2 URAMCHANSOL, 43183 |
| LEMUR 2 KADI, 43184 |
| LEMUR 2 THENICKMOLO, 43185 |
| S-NET D, 43186 |
| S-NET B, 43187 |
| S-NET A, 43188 |
| S-NET C, 43189 |
LEMUR 2 THENICKMOLO 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2024-12-26 18:02:33.159Z | 173.287° S | 2024-12-26 18:05:33.159Z | 206.124° SW | 41.401° | 2024-12-26 18:08:33.159Z | 341.584° N |
| 5 mins | 2024-12-27 07:02:33.159Z | 357.605° N | 2024-12-27 07:04:33.159Z | 307.777° NW | 38.486° | 2024-12-27 07:07:33.159Z | 209.976° SW |
Authenticating...
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