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: 8 hours ago
TLE from 8 hours ago
0 CHAMRAN-1
1 61072U 24165B 26036.78991049 .00010224 00000-0 62737-3 0 9995
2 61072 64.0767 113.8863 0042674 312.0936 47.6553 15.09815046 76816Epoch: 2026-02-05T18:57Z
TLE epoch observation values (Epoch: 2026-02-05T18:57:28.266Z)
Latitude
0.00001°
Longitude
53.58144°
Altitude
518.919 km
Speed
7.615 km/s
True Right ascension
07h 35m 32s
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
04:51:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
564.913 km
Perigee altitude
505.908 km
Semi-major axis
6,913.547 km
Eccentricity
0.00427
Inclination
64.0767°
RAAN
113.8863°
Arg. of periapsis
312.0936°
True anomaly
48.01803°
Mean anomaly
47.6553°
Eccentric anomaly
47.83653°
Mean motion
3.77565 °/min
Orbital period
95.35 mins
BSTAR
0.00062737
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-02-06 06:13:34.172Z | 166.9° S | 2026-02-06 06:15:34.172Z | 128.751° SE | 25.283° | 2026-02-06 06:18:34.172Z | 63.017° ENE |
| 5 mins | 2026-02-06 07:52:34.172Z | 275.658° WNW | 2026-02-06 07:54:34.172Z | 321.403° NNW | 22.993° | 2026-02-06 07:57:34.172Z | 9.194° NNE |
| 5 mins | 2026-02-06 14:33:34.172Z | 8.617° NNE | 2026-02-06 14:35:34.172Z | 45.5° ENE | 20.145° | 2026-02-06 14:38:34.172Z | 94.632° ESE |
| 6 mins | 2026-02-06 16:11:34.172Z | 301.251° NW | 2026-02-06 16:13:34.172Z | 256.643° W | 32.244° | 2026-02-06 16:17:34.172Z | 174.764° S |
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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