PROTOMETHEE, 58321
Orbit data source: Space-Track
PROTOMETHEE, 58321 is a payload satellite owned by Promethee (FR) in SSO that was launched on Sat, 11 Nov 2023 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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58321 intel report (Beta)
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PROTOMETHEE radio frequencies
PROTOMETHEE details
Identifier | |
Orbit | SSO |
Last TLE update | 9 hours ago |
Origin | |
Manufacturer | NanoAvionics |
Mission | Operational Commercial Imaging |
Bus & Motor | CUBESAT 16U, Unknown motor |
Mass | 30 kg wet, ~30 kg dry |
Launch date (UTC) | |
Launch vehicle | |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Box + 2 Pan, 0.4 m |
Radar Cross Section | 0.100 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 9 hours ago
0 PROTOMETHEE
1 58321U 23174BT 25015.13302931 .00008580 00000-0 37179-3 0 9992
2 58321 97.4303 92.5341 0008915 189.0849 171.0227 15.22593192 65890
Epoch: 2025-01-15T03:11Z
Definitive object data (Epoch: 2025-01-15T03:11:33.732Z)
Latitude | -0.00008° |
Longitude | -70.18619° |
Altitude | 507.172 km |
Speed | 7.607 km/s |
True Right ascension | 06h 10m 08s |
True Declination | 0° 00' 00" |
Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
Latitude | -36.2717° |
Longitude | 104.71643° |
Altitude | 506.455 km |
Speed | 7.612 km/s |
Apparent Right ascension | 20h 57m 42s |
Apparent Declination | -51° 13' 08" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 12:41:52 |
Azimuth | 125.706° SE |
Elevation | -50.225° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 501.113 km |
Perigee altitude | 488.858 km |
Semi-major axis | 6,873.123 km |
Eccentricity | 0.0008915 |
Inclination | 97.4303° |
RAAN | 92.5341° |
Arg. of periapsis | 189.0849° |
True anomaly | 171.03862° |
Mean anomaly | 171.0227° |
Eccentric anomaly | 171.03066° |
Mean motion | 3.80901 °/min |
BSTAR | 0.00037179 |
Orbital period | 94.51 mins |
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Other satellites on launch #174 in the year 2023 (2023-11-11 UTC)
PROTOMETHEE 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 | 2025-01-15 17:56:34.453Z | 9.514° NNE | 2025-01-15 17:59:34.453Z | 347.603° N | 42.95° | 2025-01-15 18:02:34.453Z | 197.373° SSW |
5 mins | 2025-01-16 04:34:34.453Z | 128.458° SE | 2025-01-16 04:36:34.453Z | 77.732° E | 29.946° | 2025-01-16 04:39:34.453Z | 9.554° NNE |
Authenticating...
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