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

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

Unknown

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago

0 SL-8 R/B
1 02802U 67045B   26008.64469324  .00000416  00000-0  12275-3 0  9999
2 02802  74.0117 100.2245 0063075 122.6007 238.1262 14.45568868 80341

Epoch: 2026-01-08T15:28Z

TLE epoch observation values (Epoch: 2026-01-08T15:28:21.495Z)

Latitude

-0.00002°

Longitude

119.9391°

Altitude

766.696 km

Speed

7.458 km/s

True Right ascension

06h 40m 53s

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

00:32:48

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

782.657 km

Perigee altitude

692.89 km

Semi-major axis

7,115.91 km

Eccentricity

0.00631

Inclination

74.0117°

RAAN

100.2245°

Arg. of periapsis

122.6007°

True anomaly

237.51496°

Mean anomaly

238.1262°

Eccentric anomaly

237.82032°

Mean motion

3.61574 °/min

Orbital period

99.56 mins

BSTAR

0.00012275

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

SL-8 DEB, 3737 (Decayed)

COSMOS 158, 2801

SL-8 DEB, 2823 (Decayed)

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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

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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.
8 mins	2026-01-09 06:32:02.718Z	165.648° S	2026-01-09 06:36:02.718Z	108.357° ESE	30.573°	2026-01-09 06:40:02.718Z	40.573° NE
6 mins	2026-01-09 08:15:02.718Z	255.414° W	2026-01-09 08:18:02.718Z	303.366° NW	22.654°	2026-01-09 08:21:02.718Z	346.959° N
7 mins	2026-01-09 16:58:02.718Z	357.841° N	2026-01-09 17:01:02.718Z	82.328° E	39.731°	2026-01-09 17:05:02.718Z	146.135° SSE

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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: 9 hours ago

TLE from 9 hours ago

TLE epoch observation values (Epoch: 2026-01-08T15:28:21.495Z)

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: 9 hours ago