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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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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 R2
1 46913U 20081J 26171.32613774 .00006378 00000-0 24964-3 0 9996
2 46913 36.8983 41.9756 0008985 306.0505 53.9411 15.25465057312462Epoch: 2026-06-20T07:49Z
TLE epoch observation values (Epoch: 2026-06-20T07:49:38.300Z)
Latitude
-0.00004°
Longitude
16.0236°
Altitude
484.869 km
Speed
7.627 km/s
True Right ascension
02h 47m 54s
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
10:58:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
498.513 km
Perigee altitude
486.167 km
Semi-major axis
6,870.477 km
Eccentricity
0.0009
Inclination
36.8983°
RAAN
41.9756°
Arg. of periapsis
306.0505°
True anomaly
54.02439°
Mean anomaly
53.9411°
Eccentric anomaly
53.98274°
Mean motion
3.81121 °/min
Orbital period
94.46 mins
BSTAR
0.00024964
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-21 20:16:13.590Z | 236.268° WSW | 2026-06-21 20:18:13.590Z | 178.631° S | 36.322° | 2026-06-21 20:21:13.590Z | 101.19° ESE |
| 6 mins | 2026-06-21 21:55:13.590Z | 255.666° W | 2026-06-21 21:57:13.590Z | 212.001° SW | 35.523° | 2026-06-21 22:01:13.590Z | 113.377° SE |
| 4 mins | 2026-06-21 23:35:13.590Z | 237.165° WSW | 2026-06-21 23:37:13.590Z | 192.767° SSW | 20.626° | 2026-06-21 23:39:13.590Z | 156.722° SSE |
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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