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

Last TLE update

5 hours ago

Origin

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

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1966-03-30 (59 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 5 hours ago

0 OV1-5 DEB
1  5361U 66025F   25200.41713515  .00005909  00000-0  14400-2 0  9994
2  5361 144.6129 258.3757 0021402  65.0001 295.2919 14.49027447320488

Epoch: 2025-07-19T10:00Z

TLE epoch observation values (Epoch: 2025-07-19T10:00:40.476Z)

Latitude

-0.00001°

Longitude

170.75253°

Altitude

721.338 km

Speed

7.5 km/s

True Right ascension

17h 13m 30s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

35.52724°

Longitude

83.16775°

Altitude

715.545 km

Speed

7.511 km/s

Apparent Right ascension

13h 34m 15s

Apparent Declination

0° 12' 11"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

04:13:01

Azimuth

52.137° ENE

Elevation

-36.011°

Doppler factor

Orbital elements

Apogee altitude

747.129 km

Perigee altitude

716.695 km

Semi-major axis

7,110.049 km

Eccentricity

0.00214

Inclination

144.6129°

RAAN

258.3757°

Arg. of periapsis

65.0001°

True anomaly

295.06991°

Mean anomaly

295.2919°

Eccentric anomaly

295.18093°

Mean motion

3.62021 °/min

Orbital period

99.44 mins

BSTAR

0.00144

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

OV1-5 DEB, 3611 (Decayed)

OV1-5 DEB, 5599

OV1-5 DEB, 27880 (Decayed)

OV1-5 DEB Visibility forecast

Observer location: undefined°, undefined°

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.
4 mins	2025-07-19 18:50:47.436Z	126.04° SE	2025-07-19 18:52:47.436Z	153.312° SSE	13.544°	2025-07-19 18:54:47.436Z	180.139° SSW
6 mins	2025-07-19 20:24:47.436Z	113.282° SE	2025-07-19 20:26:47.436Z	150.475° SSE	27.763°	2025-07-19 20:30:47.436Z	222.981° SW
7 mins	2025-07-19 21:58:47.436Z	108.274° ESE	2025-07-19 22:01:47.436Z	182.872° SSW	37.286°	2025-07-19 22:05:47.436Z	250.187° W
7 mins	2025-07-19 23:32:47.436Z	121.594° SE	2025-07-19 23:35:47.436Z	182.203° SSW	35.504°	2025-07-19 23:39:47.436Z	259.395° W
6 mins	2025-07-20 01:07:47.436Z	155.417° SSE	2025-07-20 01:10:47.436Z	209.757° SW	23.259°	2025-07-20 01:13:47.436Z	253.98° W

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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Authenticating...

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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.