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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, 0.4 m
Radar Cross Section
0.375 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 CHAMRAN-1
1 61072U 24165B   26277.50772147  .00002707  00000-0  16259-3 0  9993
2 61072  64.0762  42.4449 0062105 300.9921  58.5103 15.11786467113180
Epoch: 2026-10-04T12:11Z
TLE epoch observation values (Epoch: 2026-10-04T12:11:07.135Z)
Latitude
0.00001°
Longitude
-153.53479°
Altitude
510.497 km
Speed
7.621 km/s
True Right ascension
02h 49m 46s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
09:20:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
572.296 km
Perigee altitude
486.497 km
Semi-major axis
6,907.533 km
Eccentricity
0.00621
Inclination
64.0762°
RAAN
42.4449°
Arg. of periapsis
300.9921°
True anomaly
59.11962°
Mean anomaly
58.5103°
Eccentric anomaly
58.81472°
Mean motion
3.78058 °/min
Orbital period
95.22 mins
BSTAR
0.00016259
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Other satellites on launch #165 in the year 2024 (2024-09-14 UTC)

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