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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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: 9 hours ago
TLE from 9 hours ago
0 AFR-1
1 56964U 23084AJ 26047.60258965 .00006290 00000-0 23797-3 0 9995
2 56964 97.6065 181.6487 0011663 48.6070 311.6169 15.27257957148811Epoch: 2026-02-16T14:27Z
TLE epoch observation values (Epoch: 2026-02-16T14:27:43.745Z)
Latitude
-0.00006°
Longitude
178.12186°
Altitude
481.797 km
Speed
7.628 km/s
True Right ascension
12h 06m 35s
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
01:57:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
488.978 km
Perigee altitude
472.979 km
Semi-major axis
6,859.115 km
Eccentricity
0.00117
Inclination
97.6065°
RAAN
181.6487°
Arg. of periapsis
48.607°
True anomaly
311.51689°
Mean anomaly
311.6169°
Eccentric anomaly
311.5669°
Mean motion
3.82068 °/min
Orbital period
94.22 mins
BSTAR
0.00023797
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-17 09:28:04.916Z | 212.764° SW | 2026-02-17 09:30:04.916Z | 262.095° W | 25.516° | 2026-02-17 09:33:04.916Z | 323.522° NNW |
| 4 mins | 2026-02-17 22:29:04.916Z | 324.403° NNW | 2026-02-17 22:30:04.916Z | 302.144° NW | 20.765° | 2026-02-17 22:33:04.916Z | 239.807° WSW |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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