QAEM 100 R/B, 61071

Orbit data source: Space-Track

QAEM 100 R/B, 61071 is space debris in LEO originally from a launch on Sat, 14 Sep 2024 UTC via a QAEM-100 launch vehicle from the Sharud Missile Test Site (SMTS). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Iframe URL

https://www.satcat.com/sats-embedded/61071?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

61071, 2024-165A

Orbit

LEO

Last TLE update

11 hours ago

Origin

Islamic Revolutionary Guard Corps (IRGC) (Unknown / IRAN)

Manufacturer

IRGC

Mission

Operational spacecraft

Bus & Motor

Unknown

Mass

~200 kg wet, ~200 kg dry

Launch date (UTC)

2024-09-14 (11 months ago)

Launch vehicle

QAEM-100

Launch site

Sharud Missile Test Site (SMTS)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history

TLE from 11 hours ago

0 QAEM 100 R/B
1 61071U 24165A   25221.59136316  .00003958  00000-0  23959-3 0  9995
2 61071  64.0767 339.9550 0039103 323.1633  36.6797 15.11581293 49702

Epoch: 2025-08-09T14:11Z

TLE epoch observation values (Epoch: 2025-08-09T14:11:33.777Z)

Latitude

0.00002°

Longitude

168.73941°

Altitude

511.71 km

Speed

7.62 km/s

True Right ascension

22h 39m 49s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

-51.51891°

Longitude

24.74363°

Altitude

546.841 km

Speed

7.59 km/s

Apparent Right ascension

07h 08m 34s

Apparent Declination

-75° 44' 39"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

15:01:27

Azimuth

197.979° SSW

Elevation

-45.334°

Doppler factor

Orbital elements

Apogee altitude

557.035 km

Perigee altitude

503.009 km

Semi-major axis

6,908.159 km

Eccentricity

0.00391

Inclination

64.0767°

RAAN

339.955°

Arg. of periapsis

323.1633°

True anomaly

36.94841°

Mean anomaly

36.6797°

Eccentric anomaly

36.81395°

Mean motion

3.78007 °/min

Orbital period

95.24 mins

BSTAR

0.00023959

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

CHAMRAN-1, 61072

QAEM 100 DEB, 61181 (Decayed)

QAEM 100 R/B 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	2025-08-10 09:22:53.707Z	191.255° SSW	2025-08-10 09:25:53.707Z	132.66° SE	36.684°	2025-08-10 09:29:53.707Z	43.832° NE
4 mins	2025-08-10 11:02:53.707Z	288.059° WNW	2025-08-10 11:04:53.707Z	324.111° NNW	16.093°	2025-08-10 11:06:53.707Z	355.424° N
6 mins	2025-08-10 17:42:53.707Z	357.376° N	2025-08-10 17:44:53.707Z	37.159° NE	26.852°	2025-08-10 17:48:53.707Z	112.653° SE
4 mins	2025-08-10 19:21:53.707Z	275.928° WNW	2025-08-10 19:22:53.707Z	254.823° W	22.228°	2025-08-10 19:25:53.707Z	198.169° SSW

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 QAEM 100 R/B, 61071 on other resources

View QAEM 100 R/B, 61071 on Heavens-Above

View QAEM 100 R/B, 61071 on Keep Track

View QAEM 100 R/B, 61071 on Celestrak

View QAEM 100 R/B, 61071 on Gunter's Space Page

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