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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CHAMRAN-1 radio frequencies
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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: 2 weeks ago
TLE from 2 weeks ago
0 CHAMRAN-1
1 61072U 24165B 25250.93436862 .00005547 00000-0 36343-3 0 9992
2 61072 64.0674 248.1748 0029102 303.6436 56.1903 15.08426626 54056Epoch: 2025-09-07T22:25Z
TLE epoch observation values (Epoch: 2025-09-07T22:25:29.448Z)
Latitude
0.00003°
Longitude
-75.44461°
Altitude
531.804 km
Speed
7.604 km/s
True Right ascension
16h 32m 41s
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
20:51:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
559.787 km
Perigee altitude
519.523 km
Semi-major axis
6,917.792 km
Eccentricity
0.00291
Inclination
64.0674°
RAAN
248.1748°
Arg. of periapsis
303.6436°
True anomaly
56.46795°
Mean anomaly
56.1903°
Eccentric anomaly
56.32907°
Mean motion
3.77218 °/min
Orbital period
95.44 mins
BSTAR
0.00036343
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-19 07:00:43.953Z | 340.658° N | 2025-09-19 07:04:43.953Z | 65.875° ENE | 34.261° | 2025-09-19 07:07:43.953Z | 122.281° SE |
| 4 mins | 2025-09-19 08:40:43.953Z | 276.098° WNW | 2025-09-19 08:42:43.953Z | 241.801° WSW | 16.094° | 2025-09-19 08:44:43.953Z | 211.268° SW |
| 6 mins | 2025-09-19 22:33:43.953Z | 212.877° SW | 2025-09-19 22:35:43.953Z | 216.801° SW | 42.875° | 2025-09-19 22:39:43.953Z | 32.382° NE |
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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