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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Identifier

2802, 1967-045B

Orbit

LEO

Country

CIS

Related business

Russian Strategic Rocket Forces (RU)

Manufacturer

Yuzhnoe

Mission

Spacecraft

Bus & Motor

S3, Unknown motor

Mass

1,434 kg wet, 1,434 kg dry

Launch date (UTC)

1967-05-15 (59 years ago)

Launch vehicle

Unknown

Launch site

Plesetsk Missile And Space Complex (PKMTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

CYL, 1.1 m

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago

0 SL-8 R/B
1  2802U 67045B   26261.22692084  .00000132  00000-0  44221-4 0  9997
2  2802  74.0139 348.4783 0065184 308.8906  50.6448 14.45720429116848

Epoch: 2026-09-18T05:26Z

TLE epoch observation values (Epoch: 2026-09-18T05:26:45.960Z)

Latitude

-0.00005°

Longitude

-90.36605°

Altitude

713.038 km

Speed

7.515 km/s

True Right ascension

23h 13m 54s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow 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

03:58:32

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

783.657 km

Perigee altitude

690.894 km

Semi-major axis

7,115.413 km

Eccentricity

0.00652

Inclination

74.0139°

RAAN

348.4783°

Arg. of periapsis

308.8906°

True anomaly

51.22536°

Mean anomaly

50.6448°

Eccentric anomaly

50.93478°

Mean motion

3.61612 °/min

Orbital period

99.55 mins

BSTAR

0.000044221

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

SL-8 DEB, 2823 (Decayed)

SL-8 DEB, 3737 (Decayed)

COSMOS 158, 2801

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SL-8 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	2026-09-18 15:58:27.990Z	23.795° NE	2026-09-18 16:01:27.990Z	62.514° ENE	17.758°	2026-09-18 16:04:27.990Z	97.697° ESE
8 mins	2026-09-18 17:39:27.990Z	329.562° NNW	2026-09-18 17:43:27.990Z	227.755° WSW	59.101°	2026-09-18 17:47:27.990Z	177.049° S
7 mins	2026-09-19 06:29:27.990Z	159.717° S	2026-09-19 06:32:27.990Z	100.6° ESE	40.101°	2026-09-19 06:36:27.990Z	37.272° NE
6 mins	2026-09-19 08:11:27.990Z	260.524° W	2026-09-19 08:14:27.990Z	308.015° NW	23.509°	2026-09-19 08:17:27.990Z	347.804° N

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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-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

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

SL-8 R/B, 2802

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 6 hours ago

TLE from 6 hours ago

TLE epoch observation values (Epoch: 2026-09-18T05:26:45.960Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

SL-8 R/B Visibility forecast

Co-orbital & Co-planar RSOs

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

Documentation

Expand to show TLE details & history
Last TLE update: 6 hours ago