R2, 46913
Orbit data source: Space-Track
R2, 46913 is a payload satellite owned by NanoAvionics (LT) in LEO that was launched on Sat, 07 Nov 2020 UTC via a PSLV-DL launch vehicle from the Sirharikota (SRI). 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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46913 intel report (Beta)
R2 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 19 hours ago |
| Origin | |
| Manufacturer | NanoAvionics US |
| Mission | Operational Commercial Technology |
| Bus & Motor | CUBESAT 6U, Unknown motor |
| Mass | 6.8 kg wet, 6.8 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box, Unknown HBR |
| Radar Cross Section | 0.080 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 19 hours ago
0 R2
1 46913U 20081J 24360.65520099 .00015476 00000-0 83304-3 0 9999
2 46913 36.8999 112.3686 0010081 89.3925 270.7976 15.14150719226554Epoch: 2024-12-25T15:43Z
Definitive object data (Epoch: 2024-12-25T15:43:29.365Z)
| Latitude | 0.00002° |
| Longitude | 141.85044° |
| Altitude | 522.58 km |
| Speed | 7.604 km/s |
| True Right ascension | 07h 29m 28s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -0.09864° |
| Longitude | 136.92834° |
| Altitude | 523.334 km |
| Speed | 7.603 km/s |
| Apparent Right ascension | 04h 08m 57s |
| Apparent Declination | -40° 37' 13" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 10:04:09 |
| Azimuth | 236.121° WSW |
| Elevation | -23.927° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 533.454 km |
| Perigee altitude | 519.533 km |
| Semi-major axis | 6,904.631 km |
| Eccentricity | 0.0010081 |
| Inclination | 36.8999° |
| RAAN | 112.3686° |
| Arg. of periapsis | 89.3925° |
| True anomaly | 270.68209° |
| Mean anomaly | 270.7976° |
| Eccentric anomaly | 270.73984° |
| Mean motion | 3.78297 °/min |
| BSTAR | 0.00083304 |
| Orbital period | 95.16 mins |
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Other satellites on launch #81 in the year 2020 (2020-11-07 UTC)
R2 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 10:55:55.953Z | 195.655° SSW | 2024-12-26 10:57:55.953Z | 162.92° S | 17.799° | 2024-12-26 11:00:55.953Z | 111.096° ESE |
| 6 mins | 2024-12-26 12:35:55.953Z | 232.133° WSW | 2024-12-26 12:37:55.953Z | 181.536° SSW | 34.946° | 2024-12-26 12:41:55.953Z | 96.43° ESE |
| 6 mins | 2024-12-26 14:15:55.953Z | 254.069° W | 2024-12-26 14:17:55.953Z | 205.523° SW | 37.653° | 2024-12-26 14:21:55.953Z | 109.296° ESE |
| 5 mins | 2024-12-26 15:55:55.953Z | 248.71° W | 2024-12-26 15:57:55.953Z | 208.6° SW | 24.28° | 2024-12-26 16:00:55.953Z | 147.899° SSE |
Authenticating...
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