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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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Iframe URL

https://www.satcat.com/sats-embedded/61072?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61072, 2024-165B

Orbit

LEO

Last TLE update

9 hours ago

Origin

Iran Electronics Industries (Unknown / IRAN)

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

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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Other satellites on launch #165 in the year 2024 (2024-09-14 UTC)

QAEM 100 R/B, 61071

QAEM 100 DEB, 61181 (Decayed)

CHAMRAN-1 Visibility forecast

Observer location: undefined°, undefined°

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	2025-07-19 00:31:47.865Z	344.522° N	2025-07-19 00:35:47.865Z	63.683° ENE	29.731°	2025-07-19 00:38:47.865Z	115.64° SE
4 mins	2025-07-19 02:11:47.865Z	279.847° WNW	2025-07-19 02:13:47.865Z	241.287° WSW	19.695°	2025-07-19 02:15:47.865Z	206.804° SW
6 mins	2025-07-19 16:04:47.865Z	203.933° SW	2025-07-19 16:07:47.865Z	114.674° SE	43.897°	2025-07-19 16:10:47.865Z	37.807° NE

Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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Authenticating...

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Check out CHAMRAN-1, 61072 on other resources

View CHAMRAN-1, 61072 on NASA - NSSDCA Website

View CHAMRAN-1, 61072 on Heavens-Above

View CHAMRAN-1, 61072 on Keep Track

View CHAMRAN-1, 61072 on Celestrak

View CHAMRAN-1, 61072 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.