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: 16 hours ago
TLE from 16 hours ago
0 R2
1 46913U 20081J 25307.85094203 .00010047 00000-0 44788-3 0 9998
2 46913 36.8998 5.2689 0008646 181.6772 178.3948 15.20868592277602Epoch: 2025-11-03T20:25Z
TLE epoch observation values (Epoch: 2025-11-03T20:25:21.391Z)
Latitude
0.00001°
Longitude
15.5834°
Altitude
508.274 km
Speed
7.609 km/s
True Right ascension
00h 21m 04s
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
08:18:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
512.116 km
Perigee altitude
500.212 km
Semi-major axis
6,884.301 km
Eccentricity
0.00086
Inclination
36.8998°
RAAN
5.2689°
Arg. of periapsis
181.6772°
True anomaly
178.39757°
Mean anomaly
178.3948°
Eccentric anomaly
178.39619°
Mean motion
3.79974 °/min
Orbital period
94.74 mins
BSTAR
0.00044788
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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 | 2025-11-04 12:39:30.768Z | 247.838° W | 2025-11-04 12:41:30.768Z | 211.54° SW | 20.41° | 2025-11-04 12:44:30.768Z | 155.132° SSE |
| 5 mins | 2025-11-05 07:19:30.768Z | 201.907° SSW | 2025-11-05 07:21:30.768Z | 162.001° S | 22.251° | 2025-11-05 07:24:30.768Z | 106.06° ESE |
| 6 mins | 2025-11-05 08:58:30.768Z | 243.097° WSW | 2025-11-05 09:01:30.768Z | 152.067° SSE | 36.601° | 2025-11-05 09:04:30.768Z | 99.117° ESE |
| 5 mins | 2025-11-05 10:38:30.768Z | 254.144° W | 2025-11-05 10:40:30.768Z | 203.383° SW | 35.72° | 2025-11-05 10:43:30.768Z | 120.274° SE |
| 4 mins | 2025-11-05 12:18:30.768Z | 238.003° WSW | 2025-11-05 12:20:30.768Z | 196.99° SSW | 19.32° | 2025-11-05 12:22:30.768Z | 161.409° S |
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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