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

Country

Unknown / IRAN

Related business

Islamic Revolutionary Guard Corps (IRGC) (IR)

Manufacturer

IRGC

Mission

Operational spacecraft

Bus & Motor

Unknown

Mass

~200 kg wet, ~200 kg dry

Launch date (UTC)

2024-09-14 (1 year 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
Last TLE update: 17 hours ago

TLE from 17 hours ago

0 QAEM 100 R/B
1 61071U 24165A   25261.28189432  .00004649  00000-0  27547-3 0  9997
2 61071  64.0740 209.2941 0043267 321.4723  38.3306 15.11943302 55708

Epoch: 2025-09-18T06:45Z

TLE epoch observation values (Epoch: 2025-09-18T06:45:55.669Z)

Latitude

-0.00003°

Longitude

110.3664°

Altitude

508.84 km

Speed

7.623 km/s

True Right ascension

13h 57m 10s

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

16:25:05

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

558.804 km

Perigee altitude

499.034 km

Semi-major axis

6,907.056 km

Eccentricity

0.00433

Inclination

64.074°

RAAN

209.2941°

Arg. of periapsis

321.4723°

True anomaly

38.6394°

Mean anomaly

38.3306°

Eccentric anomaly

38.48487°

Mean motion

3.78097 °/min

Orbital period

95.21 mins

BSTAR

0.00027547

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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)

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QAEM 100 R/B Visibility forecast

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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	2025-09-19 07:07:01.931Z	330.179° NNW	2025-09-19 07:10:01.931Z	41.203° NE	44.621°	2025-09-19 07:14:01.931Z	144.771° SSE
6 mins	2025-09-19 22:37:01.931Z	236.883° WSW	2025-09-19 22:40:01.931Z	324.713° NNW	36.171°	2025-09-19 22:43:01.931Z	20.087° NNE

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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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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

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

QAEM 100 R/B, 61071

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 17 hours ago

TLE from 17 hours ago

TLE epoch observation values (Epoch: 2025-09-18T06:45:55.669Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

QAEM 100 R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out QAEM 100 R/B, 61071 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 17 hours ago