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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Iframe URL

https://www.satcat.com/sats-embedded/22797?theme=dark&initialShowStats=false

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ISO8601 Format

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, 1.6 m

Radar Cross Section

8.215 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago

0 TOS R/B
1 22797U 93058D   26076.87993619  .00000342  00000-0  63087-3 0  9991
2 22797  15.1051  96.5634 7355823  28.2424 357.1974  2.13411888246442

Epoch: 2026-03-17T21:07Z

TLE epoch observation values (Epoch: 2026-03-17T21:07:06.486Z)

Latitude

0.00028°

Longitude

-35.59583°

Altitude

724.031 km

Speed

9.828 km/s

True Right ascension

06h 26m 31s

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

21:12:44

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

37,858.966 km

Perigee altitude

361.43 km

Semi-major axis

25,488.335 km

Eccentricity

0.73558

Inclination

15.1051°

RAAN

96.5634°

Arg. of periapsis

28.2424°

True anomaly

333.65594°

Mean anomaly

357.1974°

Eccentric anomaly

349.56125°

Mean motion

0.53337 °/min

Orbital period

674.95 mins

BSTAR

0.00063087

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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, 22795 (Decayed)

STS 51 DEB, 22800 (Decayed)

STS 51 DEB, 22799 (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.
149 mins	2026-03-18 16:28:14.164Z	173.881° S	2026-03-18 16:28:14.164Z	173.881° S	26.958°	2026-03-18 18:57:14.164Z	160.157° S
45 mins	2026-03-19 07:08:14.164Z	185.777° SSW	2026-03-19 07:14:14.164Z	147.109° SSE	21.08°	2026-03-19 07:53:14.164Z	106.318° ESE
376 mins	2026-03-19 10:12:14.164Z	111.362° ESE	2026-03-19 14:47:14.164Z	146.84° SSE	22.501°	2026-03-19 16:28:14.164Z	152.66° 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: 19 hours ago

TLE from 19 hours ago

TLE epoch observation values (Epoch: 2026-03-17T21:07:06.486Z)

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: 19 hours ago