LEMUR 2 TOMATOKECHUP, 60471
Orbit data source: Space-Track
LEMUR 2 TOMATOKECHUP, 60471 is an American payload satellite in SSO that was launched on Fri, 16 Aug 2024 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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60471 intel report (Beta)
LEMUR 2 TOMATOKECHUP details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 1 day ago |
| Origin | |
| Manufacturer | Spire/Glasgow |
| Mission | Operational spacecraft |
| Bus & Motor | CUBESAT 16U, Unknown motor |
| Mass | 22 kg wet, 22 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Unknown |
| Radar Cross Section | Medium (>0.1 m² and <1 m²) |
Expand to show TLE details & history
TLE from 1 day ago
0 LEMUR 2 TOMATOKECHUP
1 60471U 24149D 24347.67180689 .00011236 00000-0 50369-3 0 9992
2 60471 97.4345 61.4566 0003037 54.9374 305.2147 15.21388388 17899Epoch: 2024-12-12T16:07Z
Definitive object data (Epoch: 2024-12-12T16:07:24.115Z)
| Latitude | 0.00006° |
| Longitude | 97.75733° |
| Altitude | 503.539 km |
| Speed | 7.613 km/s |
| True Right ascension | 04h 05m 49s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 75.22577° |
| Longitude | -51.51394° |
| Altitude | 513.148 km |
| Speed | 7.615 km/s |
| Apparent Right ascension | 10h 20m 35s |
| Apparent Declination | 33° 48' 17" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 21:05:50 |
| Azimuth | 344.051° N |
| Elevation | -14.283° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 500.706 km |
| Perigee altitude | 496.529 km |
| Semi-major axis | 6,876.754 km |
| Eccentricity | 0.0003037 |
| Inclination | 97.4345° |
| RAAN | 61.4566° |
| Arg. of periapsis | 54.9374° |
| True anomaly | 305.18626° |
| Mean anomaly | 305.2147° |
| Eccentric anomaly | 305.20048° |
| Mean motion | 3.80599 °/min |
| BSTAR | 0.00050369 |
| Orbital period | 94.59 mins |
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Other satellites on launch #149 in the year 2024 (2024-08-16 UTC)
LEMUR 2 TOMATOKECHUP 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 | 2024-12-14 04:33:54.652Z | 129.496° SE | 2024-12-14 04:36:54.652Z | 67.924° E | 25.409° | 2024-12-14 04:39:54.652Z | 11.638° NNE |
| 5 mins | 2024-12-14 17:37:54.652Z | 34.219° NE | 2024-12-14 17:39:54.652Z | 79.753° E | 32.768° | 2024-12-14 17:42:54.652Z | 165.114° S |
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