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). Payload-class satellites include a variety of spacecraft 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)
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Edit Public Description
Identifier
Orbit
Country
LT / LTURelated business
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
Shape & HBR
Box, Unknown HBR
Radar Cross Section
0.080 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 R2
1 46913U 20081J 25258.19852080 .00010938 00000-0 50495-3 0 9996
2 46913 36.8995 308.7521 0007707 131.0025 229.1390 15.19644719270040Epoch: 2025-09-15T04:45Z
TLE epoch observation values (Epoch: 2025-09-15T04:45:52.197Z)
Latitude
0.00003°
Longitude
-117.12196°
Altitude
509.496 km
Speed
7.609 km/s
True Right ascension
20h 35m 00s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
04:38:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
515.165 km
Perigee altitude
504.548 km
Semi-major axis
6,887.993 km
Eccentricity
0.00077
Inclination
36.8995°
RAAN
308.7521°
Arg. of periapsis
131.0025°
True anomaly
229.07225°
Mean anomaly
229.139°
Eccentric anomaly
229.10562°
Mean motion
3.79668 °/min
Orbital period
94.82 mins
BSTAR
0.00050495
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Other satellites on launch #81 in the year 2020 (2020-11-07 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.R2 Visibility forecast
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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 | 2025-09-16 07:50:51.252Z | 225.881° WSW | 2025-09-16 07:52:51.252Z | 184.066° SSW | 30.67° | 2025-09-16 07:56:51.252Z | 97.404° ESE |
| 5 mins | 2025-09-16 09:30:51.252Z | 250.333° W | 2025-09-16 09:32:51.252Z | 191.653° SSW | 38.839° | 2025-09-16 09:35:51.252Z | 107.773° ESE |
| 5 mins | 2025-09-16 11:10:51.252Z | 244.391° WSW | 2025-09-16 11:12:51.252Z | 189.901° SSW | 28.296° | 2025-09-16 11:15:51.252Z | 134.448° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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