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
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: 9 hours ago
TLE from 9 hours ago
0 CHAMRAN-1
1 61072U 24165B 26050.23506487 .00004871 00000-0 30405-3 0 9997
2 61072 64.0755 69.7536 0043831 311.7808 47.9564 15.09957125 78844Epoch: 2026-02-19T05:38Z
TLE epoch observation values (Epoch: 2026-02-19T05:38:29.604Z)
Latitude
-0.00008°
Longitude
-164.05906°
Altitude
518.07 km
Speed
7.616 km/s
True Right ascension
04h 39m 00s
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
17:06:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
565.278 km
Perigee altitude
504.676 km
Semi-major axis
6,913.114 km
Eccentricity
0.00438
Inclination
64.0755°
RAAN
69.7536°
Arg. of periapsis
311.7808°
True anomaly
48.33077°
Mean anomaly
47.9564°
Eccentric anomaly
48.14345°
Mean motion
3.77601 °/min
Orbital period
95.34 mins
BSTAR
0.00030405
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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 | 2026-02-20 02:26:07.206Z | 182.157° SSW | 2026-02-20 02:29:07.206Z | 128.422° SE | 30.589° | 2026-02-20 02:33:07.206Z | 49.264° ENE |
| 4 mins | 2026-02-20 04:06:07.206Z | 282.074° WNW | 2026-02-20 04:08:07.206Z | 322.716° NNW | 19.683° | 2026-02-20 04:10:07.206Z | 357.022° N |
| 5 mins | 2026-02-20 10:47:07.206Z | 7.344° NNE | 2026-02-20 10:49:07.206Z | 48.883° ENE | 23.426° | 2026-02-20 10:52:07.206Z | 101.184° ESE |
| 5 mins | 2026-02-20 12:25:07.206Z | 293.049° NW | 2026-02-20 12:27:07.206Z | 248.945° W | 27.659° | 2026-02-20 12:30:07.206Z | 188.076° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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