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: 21 hours ago

TLE from 21 hours ago

0 SL-8 R/B
1 02802U 67045B   26287.31435528  .00000163  00000-0  52751-4 0  9994
2 02802  74.0097 299.7491 0065475 254.8072 104.5839 14.45728441120617

Epoch: 2026-10-14T07:32Z

TLE epoch observation values (Epoch: 2026-10-14T07:32:40.296Z)

Latitude

-0.00002°

Longitude

163.71534°

Altitude

754.277 km

Speed

7.471 km/s

True Right ascension

19h 58m 59s

True Declination

0° 00' 00"

Sunlit

Object was in daylight 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

22:39:45

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

783.838 km

Perigee altitude

690.662 km

Semi-major axis

7,115.387 km

Eccentricity

0.00655

Inclination

74.0097°

RAAN

299.7491°

Arg. of periapsis

254.8072°

True anomaly

105.3085°

Mean anomaly

104.5839°

Eccentric anomaly

104.94635°

Mean motion

3.61614 °/min

Orbital period

99.55 mins

BSTAR

0.000052751

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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)

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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.
4 mins	2026-10-15 10:41:23.136Z	32.221° NE	2026-10-15 10:43:23.136Z	56.444° ENE	13.799°	2026-10-15 10:45:23.136Z	80.192° E
9 mins	2026-10-15 12:21:23.136Z	337.731° N	2026-10-15 12:25:23.136Z	244.773° WSW	79.466°	2026-10-15 12:30:23.136Z	167.127° S
8 mins	2026-10-16 01:11:23.136Z	153.606° SSE	2026-10-16 01:14:23.136Z	108.827° ESE	31.755°	2026-10-16 01:19:23.136Z	39.027° NE
7 mins	2026-10-16 02:53:23.136Z	250.193° W	2026-10-16 02:56:23.136Z	301.994° NW	30.844°	2026-10-16 03:00:23.136Z	356.282° 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: 21 hours ago

TLE from 21 hours ago

TLE epoch observation values (Epoch: 2026-10-14T07:32:40.296Z)

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: 21 hours ago