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 | 7 hours 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 7 hours ago
0 LEMUR 2 TOMATOKECHUP
1 60471U 24149D 24361.15338708 .00016418 00000-0 72592-3 0 9997
2 60471 97.4322 74.7698 0002097 18.5090 341.6221 15.21771513 19944Epoch: 2024-12-26T03:40Z
Definitive object data (Epoch: 2024-12-26T03:40:52.643Z)
| Latitude | -0.00013° |
| Longitude | -75.5864° |
| Altitude | 502.22 km |
| Speed | 7.614 km/s |
| True Right ascension | 04h 59m 04s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 60.16676° |
| Longitude | -88.39016° |
| Altitude | 509.697 km |
| Speed | 7.615 km/s |
| Apparent Right ascension | 00h 06m 47s |
| Apparent Declination | 18° 36' 00" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 09:36:45 |
| Azimuth | 321.564° NNW |
| Elevation | -21.839° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 498.904 km |
| Perigee altitude | 496.02 km |
| Semi-major axis | 6,875.599 km |
| Eccentricity | 0.0002097 |
| Inclination | 97.4322° |
| RAAN | 74.7698° |
| Arg. of periapsis | 18.509° |
| True anomaly | 341.61452° |
| Mean anomaly | 341.6221° |
| Eccentric anomaly | 341.61831° |
| Mean motion | 3.80695 °/min |
| BSTAR | 0.00072592 |
| Orbital period | 94.56 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2024-12-26 18:27:36.552Z | 342.22° N | 2024-12-26 18:29:36.552Z | 278.454° WNW | 32.484° | 2024-12-26 18:32:36.552Z | 218.083° SW |
| 5 mins | 2024-12-27 05:04:36.552Z | 155.065° SSE | 2024-12-27 05:06:36.552Z | 60.954° ENE | 43.307° | 2024-12-27 05:09:36.552Z | 353.503° N |
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