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: 21 hours ago
TLE from 21 hours ago
0 R2
1 46913U 20081J 26032.72805500 .00009337 00000-0 39109-3 0 9991
2 46913 36.8969 174.4797 0007081 214.2468 145.7824 15.23023349291306Epoch: 2026-02-01T17:28Z
TLE epoch observation values (Epoch: 2026-02-01T17:28:23.952Z)
Latitude
-0.00004°
Longitude
140.44632°
Altitude
499.861 km
Speed
7.614 km/s
True Right ascension
11h 37m 55s
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
16:43:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
504.545 km
Perigee altitude
494.805 km
Semi-major axis
6,877.812 km
Eccentricity
0.00071
Inclination
36.8969°
RAAN
174.4797°
Arg. of periapsis
214.2468°
True anomaly
145.828°
Mean anomaly
145.7824°
Eccentric anomaly
145.8052°
Mean motion
3.80511 °/min
Orbital period
94.61 mins
BSTAR
0.00039109
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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 | 2026-02-02 15:52:10.701Z | 258.47° W | 2026-02-02 15:55:10.701Z | 187.576° SSW | 38.139° | 2026-02-02 15:58:10.701Z | 111.804° ESE |
| 4 mins | 2026-02-02 17:33:10.701Z | 235.331° WSW | 2026-02-02 17:34:10.701Z | 211.713° SW | 23.909° | 2026-02-02 17:37:10.701Z | 147.985° SSE |
| 4 mins | 2026-02-03 12:11:10.701Z | 184.863° SSW | 2026-02-03 12:13:10.701Z | 145.247° SSE | 17.745° | 2026-02-03 12:15:10.701Z | 112.266° ESE |
| 5 mins | 2026-02-03 13:50:10.701Z | 227.685° WSW | 2026-02-03 13:52:10.701Z | 159.424° S | 34.948° | 2026-02-03 13:55:10.701Z | 99.079° ESE |
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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