SL-24 R/B, 40541

Orbit data source: Space-Track

SL-24 R/B, 40541 is space debris in SSO originally from a launch on Wed, 25 Mar 2015 UTC launched from the Orenburg, Russia (OREN). 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/40541?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

40541, 2015-014C

Orbit

SSO

Country

CIS

Related business

Federal Space Agency of Russia (Roscosmos) (RU)

Manufacturer

Yuzhnoe

Mission

Spacecraft

Bus & Motor

15A18-BR, Unknown motor

Mass

~1,000 kg wet, ~1,000 kg dry

Launch date (UTC)

2015-03-25 (11 years ago)

Launch vehicle

Unknown

Launch site

Orenburg, Russia (OREN)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 1.5 m

Radar Cross Section

10.603 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 12 hours ago

TLE from 12 hours ago

0 SL-24 R/B
1 40541U 15014C   26104.80438240  .00000216  00000-0  60085-4 0  9999
2 40541  97.3418 292.9765 0611413  64.9167 301.4161 13.77782952555065

Epoch: 2026-04-14T19:18Z

TLE epoch observation values (Epoch: 2026-04-14T19:18:18.639Z)

Latitude

-0.00002°

Longitude

160.42346°

Altitude

761.348 km

Speed

7.581 km/s

True Right ascension

19h 31m 54s

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

14:18:40

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,418.108 km

Perigee altitude

519.693 km

Semi-major axis

7,347.038 km

Eccentricity

0.06114

Inclination

97.3418°

RAAN

292.9765°

Arg. of periapsis

64.9167°

True anomaly

295.20153°

Mean anomaly

301.4161°

Eccentric anomaly

298.33261°

Mean motion

3.44647 °/min

Orbital period

104.45 mins

BSTAR

0.000060085

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Other satellites on launch #14 in the year 2015 (2015-03-25 UTC)

SL-24 DEB, 40537 (Decayed)

KOMPSAT 3A, 40536

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SL-24 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	2026-04-15 12:51:12.033Z	185.99° SSW	2026-04-15 12:54:12.033Z	243.175° WSW	37.208°	2026-04-15 12:57:12.033Z	332.171° NNW
9 mins	2026-04-16 01:29:12.033Z	6.243° NNE	2026-04-16 01:33:12.033Z	238.609° WSW	43.425°	2026-04-16 01:38:12.033Z	199.449° SSW

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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 SL-24 R/B, 40541 on other resources

View SL-24 R/B, 40541 on Heavens-Above

View SL-24 R/B, 40541 on Keep Track

View SL-24 R/B, 40541 on Celestrak

View SL-24 R/B, 40541 on Gunter's Space Page

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

SL-24 R/B, 40541

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 12 hours ago

TLE from 12 hours ago

TLE epoch observation values (Epoch: 2026-04-14T19:18:18.639Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #14 in the year 2015 (2015-03-25 UTC)

SL-24 R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out SL-24 R/B, 40541 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 12 hours ago