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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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Identifier
61072, 2024-165B
Orbit
LEO
Country
Flag of IRIR / IRAN
Related business
Manufacturer
IEI
Mission
Operational Defense Communications
Bus & Motor
Unknown
Mass
60 kg wet, 60 kg dry
Launch date (UTC)
2024-09-14 (2 years ago)
Launch vehicle
QAEM-100
Launch site
Sharud Missile Test Site (SMTS)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.3 m
Radar Cross Section
0.375 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 16 hours ago

TLE from 16 hours ago
0 CHAMRAN-1
1 61072U 24165B   26097.97623307  .00003814  00000-0  23602-3 0  9997
2 61072  64.0762 272.9554 0047540 309.8961  49.7979 15.10556360 86059
Epoch: 2026-04-07T23:25Z
TLE epoch observation values (Epoch: 2026-04-07T23:25:46.537Z)
Latitude
0.00002°
Longitude
85.26628°
Altitude
515.344 km
Speed
7.618 km/s
True Right ascension
18h 11m 49s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
21:23:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
566.004 km
Perigee altitude
500.291 km
Semi-major axis
6,911.284 km
Eccentricity
0.00475
Inclination
64.0762°
RAAN
272.9554°
Arg. of periapsis
309.8961°
True anomaly
50.21558°
Mean anomaly
49.7979°
Eccentric anomaly
50.00658°
Mean motion
3.7775 °/min
Orbital period
95.3 mins
BSTAR
0.00023602
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Other satellites on launch #165 in the year 2024 (2024-09-14 UTC)

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