TYVAK-0172, 46267
Orbit data source: Space-Track
TYVAK-0172, 46267 is a payload satellite owned by Echostar AU (US) in SSO that was launched on Sun, 30 Aug 2020 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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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46267 intel report (Beta)
TYVAK-0172 details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 10 hours ago |
| Origin | |
| Manufacturer | Tyvak NSS |
| Mission | Operational Commercial Technology |
| Bus & Motor | CUBESAT 6U?, Unknown motor |
| Mass | 11 kg wet, 11 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box + 2 Pan, Unknown HBR |
| Radar Cross Section | 0.077 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 10 hours ago
0 TYVAK-0172
1 46267U 20059C 24361.54314225 .00035183 00000-0 17120-2 0 9996
2 46267 97.7978 208.1312 0003203 31.2228 328.9195 15.18298770235798Epoch: 2024-12-26T13:02Z
Definitive object data (Epoch: 2024-12-26T13:02:07.49Z)
| Latitude | 0° |
| Longitude | -82.92104° |
| Altitude | 512.168 km |
| Speed | 7.609 km/s |
| True Right ascension | 13h 52m 31s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 13.00274° |
| Longitude | -84.31325° |
| Altitude | 511.099 km |
| Speed | 7.611 km/s |
| Apparent Right ascension | 12h 12m 02s |
| Apparent Declination | -13° 53' 20" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 21:58:09 |
| Azimuth | 302.073° NW |
| Elevation | -50.815° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 510.173 km |
| Perigee altitude | 505.762 km |
| Semi-major axis | 6,886.104 km |
| Eccentricity | 0.0003203 |
| Inclination | 97.7978° |
| RAAN | 208.1312° |
| Arg. of periapsis | 31.2228° |
| True anomaly | 328.90055° |
| Mean anomaly | 328.9195° |
| Eccentric anomaly | 328.91002° |
| Mean motion | 3.79824 °/min |
| BSTAR | 0.001712 |
| Orbital period | 94.78 mins |
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Other satellites on launch #59 in the year 2020 (2020-08-30 UTC)
| SAOCOM 1-B, 46265 |
| GNOMES-1, 46266 |
| TYVAK-0172, 46267 |
TYVAK-0172 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 | 2024-12-27 02:15:58.384Z | 44.314° NE | 2024-12-27 02:17:58.384Z | 83.164° E | 23.945° | 2024-12-27 02:20:58.384Z | 150.155° SSE |
| 5 mins | 2024-12-27 14:28:58.384Z | 204.724° SW | 2024-12-27 14:30:58.384Z | 265.014° W | 32.24° | 2024-12-27 14:33:58.384Z | 329.185° NNW |
Authenticating...
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