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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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

11 hours 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 (11 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 11 hours ago

0 SL-24 R/B
1 40303U 14070F   25129.47271807  .00000447  00000-0  10702-3 0  9995
2 40303  97.1364 146.4288 0950137 136.3583 231.6807 13.14883779503601

Epoch: 2025-05-09T11:20Z

Definitive object data (Epoch: 2025-05-09T11:20:42.841Z)

Latitude

-0.00006°

Longitude

108.72194°

Altitude

1,692.554 km

Speed

6.8 km/s

True Right ascension

09h 45m 42s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

81.97977°

Longitude

-8.85939°

Altitude

649.237 km

Speed

7.818 km/s

Apparent Right ascension

19h 44m 06s

Apparent Declination

31° 06' 10"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

06:57:50

Azimuth

349.59° N

Elevation

-18.175°

Doppler factor

Orbital elements

Apogee altitude

1,921.695 km

Perigee altitude

481.352 km

Semi-major axis

7,579.66 km

Eccentricity

0.0950137

Inclination

97.1364°

RAAN

146.4288°

Arg. of periapsis

136.3583°

True anomaly

223.75098°

Mean anomaly

231.6807°

Eccentric anomaly

227.65699°

Mean motion

3.28904 °/min

BSTAR

0.00010702

Orbital period

109.45 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.
12 mins	2025-05-10 00:14:19.785Z	138.175° SSE	2025-05-10 00:21:19.785Z	76.89° E	33.362°	2025-05-10 00:26:19.785Z	9.59° NNE
12 mins	2025-05-10 02:03:19.785Z	202.483° SSW	2025-05-10 02:09:19.785Z	256.012° W	30.369°	2025-05-10 02:15:19.785Z	326.817° NNW
4 mins	2025-05-10 13:33:19.785Z	47.497° ENE	2025-05-10 13:34:19.785Z	79.836° E	32.042°	2025-05-10 13:37:19.785Z	165.304° S

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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