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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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

10 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, 2.1 m

Radar Cross Section

10.179 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 10 hours ago

0 SL-8 R/B
1 02802U 67045B   25199.58226178  .00000213  00000-0  66673-4 0  9997
2 02802  74.0109  65.2174 0063771 129.6436 231.0373 14.45390268 55196

Epoch: 2025-07-18T13:58Z

TLE epoch observation values (Epoch: 2025-07-18T13:58:27.417Z)

Latitude

-0.00009°

Longitude

-81.02852°

Altitude

772.091 km

Speed

7.453 km/s

True Right ascension

04h 20m 52s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-21.11005°

Longitude

-88.11297°

Altitude

787.873 km

Speed

7.438 km/s

Apparent Right ascension

02h 31m 14s

Apparent Declination

-32° 05' 29"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

12:38:01

Azimuth

280.043° WNW

Elevation

-65.923°

Doppler factor

Orbital elements

Apogee altitude

783.743 km

Perigee altitude

692.977 km

Semi-major axis

7,116.497 km

Eccentricity

0.00638

Inclination

74.0109°

RAAN

65.2174°

Arg. of periapsis

129.6436°

True anomaly

230.47194°

Mean anomaly

231.0373°

Eccentric anomaly

230.75433°

Mean motion

3.6153 °/min

Orbital period

99.58 mins

BSTAR

0.000066673

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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.
9 mins	2025-07-19 02:09:20.701Z	349.861° N	2025-07-19 02:13:20.701Z	43.748° NE	39.297°	2025-07-19 02:18:20.701Z	147.396° SSE
5 mins	2025-07-19 15:02:20.701Z	122.831° SE	2025-07-19 15:04:20.701Z	94.825° ESE	16.898°	2025-07-19 15:07:20.701Z	57.12° ENE
8 mins	2025-07-19 16:41:20.701Z	221.305° SW	2025-07-19 16:45:20.701Z	296.44° NW	37.182°	2025-07-19 16:49:20.701Z	5.195° NNE

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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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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