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: 2 days ago
TLE from 2 days ago
0 CHAMRAN-1
1 61072U 24165B 25308.82165251 .00005476 00000-0 35722-3 0 9996
2 61072 64.0786 58.6876 0034563 311.8499 47.9666 15.08467769 62789Epoch: 2025-11-04T19:43Z
TLE epoch observation values (Epoch: 2025-11-04T19:43:10.776Z)
Latitude
-0.00003°
Longitude
78.58951°
Altitude
526.876 km
Speed
7.609 km/s
True Right ascension
03h 54m 45s
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
04:29:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.437 km
Perigee altitude
515.618 km
Semi-major axis
6,917.665 km
Eccentricity
0.00346
Inclination
64.0786°
RAAN
58.6876°
Arg. of periapsis
311.8499°
True anomaly
48.26163°
Mean anomaly
47.9666°
Eccentric anomaly
48.11403°
Mean motion
3.77228 °/min
Orbital period
95.43 mins
BSTAR
0.00035722
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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 | 2025-11-06 08:26:53.243Z | 177.239° S | 2025-11-06 08:29:53.243Z | 117.116° SE | 29.233° | 2025-11-06 08:32:53.243Z | 55.703° ENE |
| 4 mins | 2025-11-06 10:06:53.243Z | 284.224° WNW | 2025-11-06 10:07:53.243Z | 304.896° NW | 20.908° | 2025-11-06 10:10:53.243Z | 0.521° NNE |
| 5 mins | 2025-11-06 16:47:53.243Z | 5.995° NNE | 2025-11-06 16:49:53.243Z | 44.744° NE | 22.264° | 2025-11-06 16:52:53.243Z | 97.811° ESE |
| 6 mins | 2025-11-06 18:25:53.243Z | 298.142° NW | 2025-11-06 18:27:53.243Z | 257.817° W | 28.594° | 2025-11-06 18:31:53.243Z | 180.247° SSW |
| 6 mins | 2025-11-07 08:19:53.243Z | 177.435° S | 2025-11-07 08:21:53.243Z | 125.589° SE | 34.057° | 2025-11-07 08:25:53.243Z | 46.167° ENE |
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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