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 launched 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

IR / IRAN

Related business

Islamic Revolutionary Guard Corps (IRGC) (IR)

Manufacturer

IRGC

Mission

Spacecraft

Bus & Motor

Unknown

Mass

~200 kg wet, ~200 kg dry

Launch date (UTC)

2024-09-14 (2 years ago)

Launch vehicle

Unknown

Launch site

Sharud Missile Test Site (SMTS)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.8 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago

0 QAEM 100 R/B
1 61071U 24165A   26098.29875667  .00003295  00000-0  18115-3 0  9996
2 61071  64.0725 262.6387 0062258 309.9799  49.5860 15.14467670 86270

Epoch: 2026-04-08T07:10Z

TLE epoch observation values (Epoch: 2026-04-08T07:10:12.576Z)

Latitude

-0.00005°

Longitude

-41.47685°

Altitude

496.863 km

Speed

7.632 km/s

True Right ascension

17h 30m 33s

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

19:32:46

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

564.193 km

Perigee altitude

478.284 km

Semi-major axis

6,899.376 km

Eccentricity

0.00623

Inclination

64.0725°

RAAN

262.6387°

Arg. of periapsis

309.9799°

True anomaly

50.13193°

Mean anomaly

49.586°

Eccentric anomaly

49.85869°

Mean motion

3.78729 °/min

Orbital period

95.05 mins

BSTAR

0.00018115

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

QAEM 100 DEB, 61181 (Decayed)

CHAMRAN-1, 61072

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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.
6 mins	2026-04-08 13:40:58.404Z	253.17° W	2026-04-08 13:43:58.404Z	311.231° NW	25.729°	2026-04-08 13:46:58.404Z	8.34° NNE
4 mins	2026-04-08 20:22:58.404Z	23.454° NE	2026-04-08 20:23:58.404Z	41.776° NE	17.638°	2026-04-08 20:26:58.404Z	88.784° E
6 mins	2026-04-08 21:59:58.404Z	306.601° NW	2026-04-08 22:01:58.404Z	256.571° W	36.903°	2026-04-08 22:05:58.404Z	167.731° S
4 mins	2026-04-09 11:50:58.404Z	151.471° SSE	2026-04-09 11:52:58.404Z	103.383° ESE	23.377°	2026-04-09 11:54:58.404Z	65.835° ENE

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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: 6 hours ago

TLE from 6 hours ago

TLE epoch observation values (Epoch: 2026-04-08T07:10:12.576Z)

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: 6 hours ago