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: 6 hours ago
TLE from 6 hours ago
0 CHAMRAN-1
1 61072U 24165B 25311.87115037 .00008547 00000-0 54932-3 0 9998
2 61072 64.0792 48.7011 0034923 311.6972 48.1155 15.08519221 63240Epoch: 2025-11-07T20:54Z
TLE epoch observation values (Epoch: 2025-11-07T20:54:27.391Z)
Latitude
-0.00006°
Longitude
47.77804°
Altitude
526.6 km
Speed
7.609 km/s
True Right ascension
03h 14m 48s
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
23:08:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.528 km
Perigee altitude
515.212 km
Semi-major axis
6,917.507 km
Eccentricity
0.00349
Inclination
64.0792°
RAAN
48.7011°
Arg. of periapsis
311.6972°
True anomaly
48.41431°
Mean anomaly
48.1155°
Eccentric anomaly
48.26482°
Mean motion
3.77241 °/min
Orbital period
95.43 mins
BSTAR
0.00054932
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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 | 2025-11-08 08:10:31.437Z | 195.628° SSW | 2025-11-08 08:14:31.437Z | 97.227° ESE | 38.382° | 2025-11-08 08:17:31.437Z | 43.759° NE |
| 5 mins | 2025-11-08 16:32:31.437Z | 2.323° NNE | 2025-11-08 16:34:31.437Z | 53.204° ENE | 29.425° | 2025-11-08 16:37:31.437Z | 111.915° ESE |
| 5 mins | 2025-11-08 18:10:31.437Z | 284.483° WNW | 2025-11-08 18:12:31.437Z | 246.884° WSW | 20.761° | 2025-11-08 18:15:31.437Z | 197.603° SSW |
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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