OV1-5 DEB, 5361

Orbit data source: Space-Track

OV1-5 DEB, 5361 is space debris in LEO originally from a launch on Wed, 30 Mar 1966 UTC launched from the Air Force Western Test Range (AFWTR). 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/5361?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

5361, 1966-025F

Orbit

LEO

Country

Related business

Air Force Systems Command (OAR legacy assets) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-03-30 (60 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago

0 OV1-5 DEB
1  5361U 66025F   26077.84451339  .00007789  00000-0  16953-2 0  9990
2  5361 144.6117 175.1754 0018976 205.0810 154.8966 14.54908299355663

Epoch: 2026-03-18T20:16Z

TLE epoch observation values (Epoch: 2026-03-18T20:16:05.956Z)

Latitude

-0.00004°

Longitude

54.74819°

Altitude

720.823 km

Speed

7.491 km/s

True Right ascension

11h 40m 42s

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

07:27:02

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

726.211 km

Perigee altitude

699.3 km

Semi-major axis

7,090.893 km

Eccentricity

0.0019

Inclination

144.6117°

RAAN

175.1754°

Arg. of periapsis

205.081°

True anomaly

154.98866°

Mean anomaly

154.8966°

Eccentric anomaly

154.94265°

Mean motion

3.63489 °/min

Orbital period

99.04 mins

BSTAR

0.0016953

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Other satellites on launch #25 in the year 1966 (1966-03-30 UTC)

OV1-5 DEB, 27880 (Decayed)

OV1-5 DEB, 3611 (Decayed)

OV1-5 DEB, 5599

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OV1-5 DEB 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.
7 mins	2026-03-19 03:05:50.733Z	137.766° SSE	2026-03-19 03:09:50.733Z	208.248° SW	27.4°	2026-03-19 03:12:50.733Z	255.568° W
6 mins	2026-03-19 23:05:50.733Z	109.17° ESE	2026-03-19 23:08:50.733Z	166.105° S	27.687°	2026-03-19 23:11:50.733Z	218.878° SW
7 mins	2026-03-20 00:39:50.733Z	107.964° ESE	2026-03-20 00:42:50.733Z	181.529° SSW	37.185°	2026-03-20 00:46:50.733Z	249.51° W
7 mins	2026-03-20 02:13:50.733Z	123.66° SE	2026-03-20 02:16:50.733Z	197.241° SSW	35.771°	2026-03-20 02:20:50.733Z	260.956° W

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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 OV1-5 DEB, 5361 on other resources

View OV1-5 DEB, 5361 on Heavens-Above

View OV1-5 DEB, 5361 on Keep Track

View OV1-5 DEB, 5361 on Celestrak

View OV1-5 DEB, 5361 on Gunter's Space Page

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

OV1-5 DEB, 5361

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 6 hours ago

TLE from 6 hours ago

TLE epoch observation values (Epoch: 2026-03-18T20:16:05.956Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #25 in the year 1966 (1966-03-30 UTC)

OV1-5 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out OV1-5 DEB, 5361 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 6 hours ago