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: 11 hours ago
TLE from 11 hours ago
0 CHAMRAN-1
1 61072U 24165B 25323.86918177 .00006430 00000-0 41380-3 0 9998
2 61072 64.0791 9.3995 0036012 312.0789 47.7263 15.08725829 65054Epoch: 2025-11-19T20:51Z
TLE epoch observation values (Epoch: 2025-11-19T20:51:37.304Z)
Latitude
-0.0001°
Longitude
-2.64071°
Altitude
525.344 km
Speed
7.61 km/s
True Right ascension
00h 37m 35s
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
04:54:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
563.647 km
Perigee altitude
513.829 km
Semi-major axis
6,916.875 km
Eccentricity
0.0036
Inclination
64.0791°
RAAN
9.3995°
Arg. of periapsis
312.0789°
True anomaly
48.03257°
Mean anomaly
47.7263°
Eccentric anomaly
47.87934°
Mean motion
3.77293 °/min
Orbital period
95.42 mins
BSTAR
0.0004138
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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 | 2025-11-20 13:17:28.079Z | 343.731° N | 2025-11-20 13:20:28.079Z | 37.311° NE | 32.848° | 2025-11-20 13:24:28.079Z | 122.028° SE |
| 4 mins | 2025-11-20 14:57:28.079Z | 271.993° WNW | 2025-11-20 14:58:28.079Z | 254.326° W | 17.311° | 2025-11-20 15:01:28.079Z | 206.243° SW |
| 6 mins | 2025-11-21 04:50:28.079Z | 209.172° SW | 2025-11-21 04:52:28.079Z | 151.02° SSE | 44.906° | 2025-11-21 04:56:28.079Z | 33.816° 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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