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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: 9 hours ago

TLE from 9 hours ago
0 CHAMRAN-1
1 61072U 24165B   26140.20966831  .00002675  00000-0  16723-3 0  9994
2 61072  64.0742 134.1546 0051459 308.3437  51.3059 15.10835370 92431
Epoch: 2026-05-20T05:01Z
TLE epoch observation values (Epoch: 2026-05-20T05:01:55.341Z)
Latitude
-0.00003°
Longitude
-179.1985°
Altitude
513.49 km
Speed
7.62 km/s
True Right ascension
08h 56m 37s
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
22:44:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
567.857 km
Perigee altitude
496.736 km
Semi-major axis
6,910.433 km
Eccentricity
0.00515
Inclination
64.0742°
RAAN
134.1546°
Arg. of periapsis
308.3437°
True anomaly
51.76799°
Mean anomaly
51.3059°
Eccentric anomaly
51.53676°
Mean motion
3.7782 °/min
Orbital period
95.28 mins
BSTAR
0.00016723
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Other satellites on launch #165 in the year 2024 (2024-09-14 UTC)

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