KHAYYAM, 53370
Orbit data source: Space-Track
KHAYYAM, 53370 is an Iranian payload satellite in SSO that was launched on Tue, 09 Aug 2022 UTC via a SOYUZ-2-1B launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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53370 intel report (Beta)
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Identifier
Orbit
Country
IR / IRANRelated business
Manufacturer
VNIIEM
Mission
Operational Civil Imaging
Bus & Motor
KANOPUS?, Unknown motor
Mass
650 kg wet, 650 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 3.0 m
Radar Cross Section
1.665 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 KHAYYAM
1 53370U 22096A 26171.44105519 .00003761 00000-0 15001-3 0 9990
2 53370 97.3437 75.6072 0002369 74.2148 285.9352 15.25788386215089Epoch: 2026-06-20T10:35Z
TLE epoch observation values (Epoch: 2026-06-20T10:35:07.168Z)
Latitude
0.00003°
Longitude
8.17169°
Altitude
491.073 km
Speed
7.62 km/s
True Right ascension
05h 02m 25s
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
21:25:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
487.001 km
Perigee altitude
483.749 km
Semi-major axis
6,863.512 km
Eccentricity
0.00024
Inclination
97.3437°
RAAN
75.6072°
Arg. of periapsis
74.2148°
True anomaly
285.90909°
Mean anomaly
285.9352°
Eccentric anomaly
285.92215°
Mean motion
3.81701 °/min
Orbital period
94.31 mins
BSTAR
0.00015001
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Other satellites on launch #96 in the year 2022 (2022-08-09 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.KHAYYAM 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 | 2026-06-22 17:48:00.942Z | 175.409° S | 2026-06-22 17:51:00.942Z | 276.554° WNW | 43.245° | 2026-06-22 17:54:00.942Z | 342.761° N |
| 5 mins | 2026-06-23 06:50:00.942Z | 352.768° N | 2026-06-23 06:52:00.942Z | 301.914° NW | 35.798° | 2026-06-23 06:55:00.942Z | 214.843° SW |
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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