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 25288.87496453 .00010351 00000-0 46763-3 0 9994
2 46913 36.8974 121.3217 0008478 9.4714 350.6192 15.20401203274716Epoch: 2025-10-15T20:59Z
TLE epoch observation values (Epoch: 2025-10-15T20:59:56.935Z)
Latitude
-0.00001°
Longitude
141.69169°
Altitude
497.983 km
Speed
7.621 km/s
True Right ascension
08h 05m 17s
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
22:24:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
513.411 km
Perigee altitude
501.736 km
Semi-major axis
6,885.711 km
Eccentricity
0.00085
Inclination
36.8974°
RAAN
121.3217°
Arg. of periapsis
9.4714°
True anomaly
350.60335°
Mean anomaly
350.6192°
Eccentric anomaly
350.61128°
Mean motion
3.79857 °/min
Orbital period
94.77 mins
BSTAR
0.00046763
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-16 16:07:46.242Z | 190.071° SSW | 2025-10-16 16:09:46.242Z | 155.381° SSE | 16.674° | 2025-10-16 16:11:46.242Z | 119.643° SE |
| 6 mins | 2025-10-16 17:46:46.242Z | 232.71° WSW | 2025-10-16 17:48:46.242Z | 190.074° SSW | 33.128° | 2025-10-16 17:52:46.242Z | 97.296° ESE |
| 5 mins | 2025-10-16 19:26:46.242Z | 251.949° W | 2025-10-16 19:28:46.242Z | 192.347° SSW | 38.275° | 2025-10-16 19:31:46.242Z | 111.57° ESE |
| 5 mins | 2025-10-16 21:06:46.242Z | 240.337° WSW | 2025-10-16 21:08:46.242Z | 190.332° SSW | 24.793° | 2025-10-16 21:11:46.242Z | 140.396° 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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