SL-24 R/B, 40303

Orbit data source: Space-Track

SL-24 R/B, 40303 is space debris in SSO originally from a launch on Thu, 06 Nov 2014 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/40303?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

40303, 2014-070F

Orbit

SSO

Last TLE update

1 day ago

Origin

Federal Space Agency of Russia (Roscosmos) (CIS)

Manufacturer

Yuzhnoe

Mission

Spacecraft

Bus & Motor

15A18-BR, Unknown motor

Mass

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

Launch date (UTC)

2014-11-06 (10 years ago)

Launch vehicle

Unknown

Launch site

Orenburg, Russia (OREN)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 3 m

Radar Cross Section

10.603 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 SL-24 R/B
1 40303U 14070F   25114.48078340  .00000523  00000-0  12641-3 0  9996
2 40303  97.1384 136.1233 0949509 174.6379 186.5849 13.14866389501596

Epoch: 2025-04-24T11:32Z

Definitive object data (Epoch: 2025-04-24T11:32:19.685Z)

Latitude

-0.00009°

Longitude

110.28969°

Altitude

1,923.38 km

Speed

6.595 km/s

True Right ascension

09h 04m 29s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-53.56481°

Longitude

-78.60826°

Altitude

839.427 km

Speed

7.619 km/s

Apparent Right ascension

15h 15m 45s

Apparent Declination

-71° 02' 42"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

23:19:11

Azimuth

204.268° SW

Elevation

-47.277°

Doppler factor

Orbital elements

Apogee altitude

1,921.292 km

Perigee altitude

481.888 km

Semi-major axis

7,579.727 km

Eccentricity

0.0949509

Inclination

97.1384°

RAAN

136.1233°

Arg. of periapsis

174.6379°

True anomaly

185.4693°

Mean anomaly

186.5849°

Eccentric anomaly

186.01483°

Mean motion

3.28899 °/min

BSTAR

0.00012641

Orbital period

109.46 mins

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Other satellites on launch #70 in the year 2014 (2014-11-06 UTC)

ASNARO, 40298

HODOYOSHI 1, 40299 (Decayed)

CHUBUSAT 1, 40300 (Decayed)

QSAT-EOS, 40301 (Decayed)

TSUBAME, 40302 (Decayed)

SL-24 PLAT, 40304 (Decayed)

SL-24 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.
15 mins	2025-04-26 00:10:57.827Z	130.213° SE	2025-04-26 00:19:57.827Z	63.433° ENE	31.851°	2025-04-26 00:25:57.827Z	9.118° NNE
16 mins	2025-04-26 01:58:57.827Z	188.055° SSW	2025-04-26 02:06:57.827Z	250.981° W	39.589°	2025-04-26 02:14:57.827Z	337.164° NNW
4 mins	2025-04-26 13:32:57.827Z	51.174° ENE	2025-04-26 13:34:57.827Z	98.208° ESE	24.979°	2025-04-26 13:36:57.827Z	143.033° SSE

Authenticating...

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Check out SL-24 R/B, 40303 on other resources

View SL-24 R/B, 40303 on Heavens-Above

View SL-24 R/B, 40303 on Keep Track

View SL-24 R/B, 40303 on Celestrak

View SL-24 R/B, 40303 on Gunter's Space Page

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