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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Identifier
Orbit
Country
IR / 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, 0.4 m
Radar Cross Section
0.375 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 CHAMRAN-1
1 61072U 24165B 26306.87562377 .00003654 00000-0 21318-3 0 9992
2 61072 64.0756 305.7431 0064246 299.3899 60.0812 15.12011189117623Epoch: 2026-11-02T21:00Z
TLE epoch observation values (Epoch: 2026-11-02T21:00:53.893Z)
Latitude
-0.00002°
Longitude
-51.62783°
Altitude
510.109 km
Speed
7.622 km/s
True Right ascension
20h 22m 58s
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
23:52:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
573.086 km
Perigee altitude
484.338 km
Semi-major axis
6,906.849 km
Eccentricity
0.00642
Inclination
64.0756°
RAAN
305.7431°
Arg. of periapsis
299.3899°
True anomaly
60.72185°
Mean anomaly
60.0812°
Eccentric anomaly
60.40127°
Mean motion
3.78114 °/min
Orbital period
95.21 mins
BSTAR
0.00021318
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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 | 2026-11-03 10:14:01.698Z | 341.903° N | 2026-11-03 10:18:01.698Z | 67.048° ENE | 41.706° | 2026-11-03 10:21:01.698Z | 121.089° SE |
| 4 mins | 2026-11-03 11:54:01.698Z | 272.744° WNW | 2026-11-03 11:55:01.698Z | 255.49° W | 18.139° | 2026-11-03 11:58:01.698Z | 207.493° SW |
| 6 mins | 2026-11-04 01:45:01.698Z | 208.265° SW | 2026-11-04 01:47:01.698Z | 156.548° SSE | 83.503° | 2026-11-04 01:51:01.698Z | 34.066° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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