SL-8 R/B, 2802

Orbit data source: Space-Track

SL-8 R/B, 2802 is space debris in LEO originally from a launch on Mon, 15 May 1967 UTC launched from the Plesetsk Missile And Space Complex (PKMTR). 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/2802?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

2802, 1967-045B

Orbit

LEO

Last TLE update

16 hours ago

Origin

Russian Strategic Rocket Forces (CIS)

Manufacturer

Yuzhnoe

Mission

Spacecraft

Bus & Motor

S3, Unknown motor

Mass

1,434 kg wet, 1,434 kg dry

Launch date (UTC)

1967-05-15 (58 years ago)

Launch vehicle

Unknown

Launch site

Plesetsk Missile And Space Complex (PKMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 4.2 m

Radar Cross Section

10.179 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 16 hours ago

0 SL-8 R/B
1 02802U 67045B   25132.85946784  .00000270  00000-0  82869-4 0  9994
2 02802  74.0114 189.7733 0065791 269.7420  89.6198 14.45357463 45559

Epoch: 2025-05-12T20:37Z

Definitive object data (Epoch: 2025-05-12T20:37:38.021Z)

Latitude

-0.00008°

Longitude

9.49835°

Altitude

743.471 km

Speed

7.483 km/s

True Right ascension

12h 39m 05s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at TLE epoch

Visualization TLE readout

Latitude

-53.28767°

Longitude

-14.24156°

Altitude

722.92 km

Speed

7.513 km/s

Apparent Right ascension

10h 10m 44s

Apparent Declination

-47° 27' 37"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

21:24:29

Azimuth

224.048° SW

Elevation

-78.76°

Doppler factor

Orbital elements

Apogee altitude

785.289 km

Perigee altitude

691.647 km

Semi-major axis

7,116.605 km

Eccentricity

0.0065791

Inclination

74.0114°

RAAN

189.7733°

Arg. of periapsis

269.742°

True anomaly

90.37371°

Mean anomaly

89.6198°

Eccentric anomaly

89.99675°

Mean motion

3.61521 °/min

BSTAR

0.000082869

Orbital period

99.58 mins

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Other satellites on launch #45 in the year 1967 (1967-05-15 UTC)

COSMOS 158, 2801

SL-8 DEB, 2823 (Decayed)

SL-8 DEB, 3737 (Decayed)

SL-8 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.
6 mins	2025-05-13 13:47:48.797Z	17.439° NNE	2025-05-13 13:50:48.797Z	54.406° ENE	17.525°	2025-05-13 13:53:48.797Z	93.626° ESE
9 mins	2025-05-13 15:28:48.797Z	330.029° NNW	2025-05-13 15:32:48.797Z	259.899° W	40.174°	2025-05-13 15:37:48.797Z	178.045° S
8 mins	2025-05-14 04:18:48.797Z	167.227° S	2025-05-14 04:22:48.797Z	92.397° ESE	34.347°	2025-05-14 04:26:48.797Z	34.949° NE
6 mins	2025-05-14 06:01:48.797Z	264.42° W	2025-05-14 06:03:48.797Z	294.068° NW	21.461°	2025-05-14 06:07:48.797Z	348.543° N

Authenticating...

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Check out SL-8 R/B, 2802 on other resources

View SL-8 R/B, 2802 on Heavens-Above

View SL-8 R/B, 2802 on Keep Track

View SL-8 R/B, 2802 on Celestrak

View SL-8 R/B, 2802 on Gunter's Space Page

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