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, Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 R2
1 46913U 20081J 26123.27279409 .00008897 00000-0 35362-3 0 9992
2 46913 36.8994 337.8880 0008220 265.7118 94.2691 15.24795757305127Epoch: 2026-05-03T06:32Z
TLE epoch observation values (Epoch: 2026-05-03T06:32:49.409Z)
Latitude
-0.00004°
Longitude
18.50336°
Altitude
490.931 km
Speed
7.621 km/s
True Right ascension
22h 31m 33s
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
01:33:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
499.998 km
Perigee altitude
488.699 km
Semi-major axis
6,872.485 km
Eccentricity
0.00082
Inclination
36.8994°
RAAN
337.888°
Arg. of periapsis
265.7118°
True anomaly
94.36303°
Mean anomaly
94.2691°
Eccentric anomaly
94.31606°
Mean motion
3.80954 °/min
Orbital period
94.5 mins
BSTAR
0.00035362
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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 | 2026-05-03 19:25:15.494Z | 233.844° WSW | 2026-05-03 19:27:15.494Z | 183.6° SSW | 34.841° | 2026-05-03 19:30:15.494Z | 102.025° ESE |
| 6 mins | 2026-05-03 21:04:15.494Z | 256.581° W | 2026-05-03 21:07:15.494Z | 164.055° S | 36.862° | 2026-05-03 21:10:15.494Z | 111.234° ESE |
| 5 mins | 2026-05-03 22:44:15.494Z | 242.73° WSW | 2026-05-03 22:46:15.494Z | 197.487° SSW | 23.188° | 2026-05-03 22:49:15.494Z | 144.946° SSE |
| 4 mins | 2026-05-04 17:21:15.494Z | 187.741° SSW | 2026-05-04 17:23:15.494Z | 147.386° SSE | 18.408° | 2026-05-04 17:25:15.494Z | 112.891° 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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