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: 1 day ago
TLE from 1 day ago
0 AFR-1
1 56964U 23084AJ 25305.62194023 .00006420 00000-0 25457-3 0 9997
2 56964 97.5985 72.7639 0012293 63.4561 296.7935 15.25677184132497Epoch: 2025-11-01T14:55Z
TLE epoch observation values (Epoch: 2025-11-01T14:55:35.635Z)
Latitude
-0.00008°
Longitude
167.71605°
Altitude
488.047 km
Speed
7.623 km/s
True Right ascension
04h 51m 03s
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
11:26:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
494.157 km
Perigee altitude
477.282 km
Semi-major axis
6,863.856 km
Eccentricity
0.00123
Inclination
97.5985°
RAAN
72.7639°
Arg. of periapsis
63.4561°
True anomaly
296.66767°
Mean anomaly
296.7935°
Eccentric anomaly
296.73059°
Mean motion
3.81673 °/min
Orbital period
94.32 mins
BSTAR
0.00025457
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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 | 2025-11-02 21:23:46.693Z | 17.138° NNE | 2025-11-02 21:26:46.693Z | 127.743° SE | 43.67° | 2025-11-02 21:29:46.693Z | 186.938° SSW |
| 4 mins | 2025-11-03 08:00:46.693Z | 107.847° ESE | 2025-11-03 08:01:46.693Z | 83.626° E | 23.015° | 2025-11-03 08:04:46.693Z | 17.405° NNE |
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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