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: 7 hours ago

TLE from 7 hours ago

0 SL-8 R/B
1 02802U 67045B   26107.88142315  .00000199  00000-0  62746-4 0  9990
2 02802  74.0096 274.8909 0065176 272.7622  86.6077 14.45651036 94688

Epoch: 2026-04-17T21:09Z

TLE epoch observation values (Epoch: 2026-04-17T21:09:14.960Z)

Latitude

-0.00002°

Longitude

111.57031°

Altitude

740.066 km

Speed

7.486 km/s

True Right ascension

18h 19m 33s

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

11:17:47

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

783.881 km

Perigee altitude

691.127 km

Semi-major axis

7,115.641 km

Eccentricity

0.00652

Inclination

74.0096°

RAAN

274.8909°

Arg. of periapsis

272.7622°

True anomaly

87.35359°

Mean anomaly

86.6077°

Eccentric anomaly

86.98061°

Mean motion

3.61595 °/min

Orbital period

99.56 mins

BSTAR

0.000062746

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

COSMOS 158, 2801

SL-8 DEB, 3737 (Decayed)

SL-8 DEB, 2823 (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.
9 mins	2026-04-18 12:13:00.621Z	192.315° SSW	2026-04-18 12:18:00.621Z	55.902° ENE	43.716°	2026-04-18 12:22:00.621Z	22.051° NNE
4 mins	2026-04-18 20:59:00.621Z	32.889° NE	2026-04-18 21:01:00.621Z	58.985° ENE	15.604°	2026-04-18 21:03:00.621Z	84.194° E
8 mins	2026-04-18 22:39:00.621Z	332.757° NNW	2026-04-18 22:43:00.621Z	236.575° WSW	42.441°	2026-04-18 22:47:00.621Z	174.381° S

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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: 7 hours ago

TLE from 7 hours ago

TLE epoch observation values (Epoch: 2026-04-17T21:09:14.960Z)

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: 7 hours ago