AFR-1, 56964
Orbit data source: Space-Track
AFR-1, 56964 is a payload satellite owned by Azista BST (IN) in SSO that was launched on Mon, 12 Jun 2023 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). 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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56964 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
IN / INDRelated business
Manufacturer
Azista BST
Mission
Operational Commercial Imaging
Bus & Motor
AFR, Unknown motor
Mass
80 kg wet, 80 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 0.5 m
Radar Cross Section
1.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 AFR-1
1 56964U 23084AJ 25260.94644976 .00005002 00000-0 20377-3 0 9990
2 56964 97.5922 27.4231 0010686 210.8437 149.2174 15.24900924125687Epoch: 2025-09-17T22:42Z
TLE epoch observation values (Epoch: 2025-09-17T22:42:53.259Z)
Latitude
0.00003°
Longitude
49.58608°
Altitude
500.484 km
Speed
7.611 km/s
True Right ascension
01h 49m 41s
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
22:16:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
495.388 km
Perigee altitude
480.713 km
Semi-major axis
6,866.187 km
Eccentricity
0.00107
Inclination
97.5922°
RAAN
27.4231°
Arg. of periapsis
210.8437°
True anomaly
149.28°
Mean anomaly
149.2174°
Eccentric anomaly
149.24871°
Mean motion
3.81478 °/min
Orbital period
94.37 mins
BSTAR
0.00020377
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Other satellites on launch #84 in the year 2023 (2023-06-12 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.AFR-1 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 | 2025-09-18 08:17:56.328Z | 148.613° SSE | 2025-09-18 08:20:56.328Z | 51.618° ENE | 38.199° | 2025-09-18 08:23:56.328Z | 358.066° N |
| 6 mins | 2025-09-18 21:19:56.328Z | 16.784° NNE | 2025-09-18 21:22:56.328Z | 163.197° S | 42.141° | 2025-09-18 21:25:56.328Z | 188.548° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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