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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
Last TLE update
9 hours ago
Origin
Manufacturer
IEI
Mission
Operational Defense Communications
Bus & Motor
Unknown
Mass
60 kg wet, 60 kg dry
Launch date (UTC)
2024-09-14 (10 months 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

TLE from 9 hours ago
0 CHAMRAN-1
1 61072U 24165B   25199.60269139  .00002908  00000-0  20014-3 0  9995
2 61072  64.0899  56.0860 0025618 315.0768  44.8273 15.07818730 46313
Epoch: 2025-07-18T14:27Z
TLE epoch observation values (Epoch: 2025-07-18T14:27:52.536Z)
Latitude
0.00004°
Longitude
-97.53467°
Altitude
532.276 km
Speed
7.604 km/s
True Right ascension
03h 44m 20s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-59.84587°
Longitude
137.49555°
Altitude
556.327 km
Speed
7.587 km/s
Apparent Right ascension
22h 21m 15s
Apparent Declination
-56° 04' 46"
Sunlit
Object is in full shadow
Visualization observer readout
Local Sidereal Time
12:20:25
Azimuth
139.592° SSE
Elevation
-64.676°
Doppler factor
1
Orbital elements
Apogee altitude
559.239 km
Perigee altitude
523.785 km
Semi-major axis
6,919.649 km
Eccentricity
0.00256
Inclination
64.0899°
RAAN
56.086°
Arg. of periapsis
315.0768°
True anomaly
45.03472°
Mean anomaly
44.8273°
Eccentric anomaly
44.93096°
Mean motion
3.77066 °/min
Orbital period
95.47 mins
BSTAR
0.00020014
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