CHAMRAN-1, 61072
Orbit data source: Space-Track
CHAMRAN-1, 61072 is an Iranian payload satellite in LEO that was launched on Sat, 14 Sep 2024 UTC via a QAEM-100 launch vehicle from the Sharud Missile Test Site (SMTS). 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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61072 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
Unknown / IRANRelated business
Manufacturer
IEI
Mission
Operational Defense Communications
Bus & Motor
Unknown
Mass
60 kg wet, 60 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.375 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 CHAMRAN-1
1 61072U 24165B 25294.83263500 .00006980 00000-0 45460-3 0 9998
2 61072 64.0757 104.4954 0033020 311.1417 48.6848 15.08279978 60673Epoch: 2025-10-21T19:58Z
TLE epoch observation values (Epoch: 2025-10-21T19:58:59.664Z)
Latitude
-0.00008°
Longitude
134.23184°
Altitude
528.375 km
Speed
7.608 km/s
True Right ascension
06h 57m 58s
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
21:51:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
562.946 km
Perigee altitude
517.258 km
Semi-major axis
6,918.239 km
Eccentricity
0.0033
Inclination
64.0757°
RAAN
104.4954°
Arg. of periapsis
311.1417°
True anomaly
48.96977°
Mean anomaly
48.6848°
Eccentric anomaly
48.82721°
Mean motion
3.77181 °/min
Orbital period
95.44 mins
BSTAR
0.0004546
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Other satellites on launch #165 in the year 2024 (2024-09-14 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.CHAMRAN-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 | 2025-10-22 13:39:26.859Z | 236.623° WSW | 2025-10-22 13:41:26.859Z | 281.452° WNW | 37.122° | 2025-10-22 13:45:26.859Z | 22.089° NNE |
| 7 mins | 2025-10-22 21:59:26.859Z | 327.172° NNW | 2025-10-22 22:02:26.859Z | 151.546° SSE | 44.885° | 2025-10-22 22:06:26.859Z | 148.528° SSE |
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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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