TOS R/B, 22797

Orbit data source: Space-Track

TOS R/B, 22797 is space debris in HEO originally from an American launch on Sun, 12 Sep 1993 UTC launched from the Air Force Eastern Test Range (AFETR). 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/22797?theme=dark&initialShowStats=false

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Identifier

22797, 1993-058D

Orbit

HEO

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

MMA/CSD

Mission

Spacecraft

Bus & Motor

ORBUS 21, Unknown motor

Mass

9,366 kg wet, 1,195 kg dry

Launch date (UTC)

1993-09-12 (33 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl + Cone, 1.8 m

Radar Cross Section

8.215 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago

0 TOS R/B
1 22797U 93058D   26256.68494603  .00000977  00000-0  14674-2 0  9990
2 22797  15.3388  31.8715 7365737 150.7892 286.9822  2.13550998250288

Epoch: 2026-09-13T16:26Z

TLE epoch observation values (Epoch: 2026-09-13T16:26:19.336Z)

Latitude

-0.00019°

Longitude

152.66091°

Altitude

26,171.113 km

Speed

2.974 km/s

True Right ascension

02h 07m 40s

True Declination

0° 00' 01"

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

08:13:16

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

37,865.03 km

Perigee altitude

333.247 km

Semi-major axis

25,477.276 km

Eccentricity

0.73657

Inclination

15.3388°

RAAN

31.8715°

Arg. of periapsis

150.7892°

True anomaly

209.37757°

Mean anomaly

286.9822°

Eccentric anomaly

247.88459°

Mean motion

0.53372 °/min

Orbital period

674.51 mins

BSTAR

0.0014674

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Other satellites on launch #58 in the year 1993 (1993-09-12 UTC)

ACTS, 22796

ORFEUS-SPAS, 22798 (Decayed)

STS 51 DEB, 22800 (Decayed)

STS 51 DEB, 22799 (Decayed)

STS 51, 22795 (Decayed)

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TOS 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.
10 mins	2026-09-14 16:51:13.285Z	243.546° WSW	2026-09-14 16:57:13.285Z	225.65° WSW	12.687°	2026-09-14 17:01:13.285Z	201.237° SSW
608 mins	2026-09-15 05:21:13.285Z	208.293° SW	2026-09-15 08:12:13.285Z	207.092° SW	27.994°	2026-09-15 15:29:13.285Z	156.739° 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 TOS R/B, 22797 on other resources

View TOS R/B, 22797 on Heavens-Above

View TOS R/B, 22797 on Keep Track

View TOS R/B, 22797 on Celestrak

View TOS R/B, 22797 on Gunter's Space Page

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

TOS R/B, 22797

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 23 hours ago

TLE from 23 hours ago

TLE epoch observation values (Epoch: 2026-09-13T16:26:19.336Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #58 in the year 1993 (1993-09-12 UTC)

TOS R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out TOS R/B, 22797 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 23 hours ago