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

22 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 22 hours ago

0 OV1-5 DEB
1 05361U 66025F   25129.14790434  .00009807  00000-0  24881-2 0  9994
2 05361 144.6127 221.5453 0021877 228.6354 131.2459 14.48175441310074

Epoch: 2025-05-09T03:32Z

Definitive object data (Epoch: 2025-05-09T03:32:58.934Z)

Latitude

-0.00006°

Longitude

-58.90838°

Altitude

740.868 km

Speed

7.481 km/s

True Right ascension

14h 46m 10s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at TLE epoch

Visualization TLE readout

Latitude

31.22376°

Longitude

-175.71252°

Altitude

739.088 km

Speed

7.486 km/s

Apparent Right ascension

03h 26m 12s

Apparent Declination

-5° 33' 38"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

09:47:59

Azimuth

269.205° W

Elevation

-7.735°

Doppler factor

Orbital elements

Apogee altitude

750.259 km

Perigee altitude

719.137 km

Semi-major axis

7,112.835 km

Eccentricity

0.0021877

Inclination

144.6127°

RAAN

221.5453°

Arg. of periapsis

228.6354°

True anomaly

131.43405°

Mean anomaly

131.2459°

Eccentric anomaly

131.34001°

Mean motion

3.61809 °/min

BSTAR

0.0024881

Orbital period

99.5 mins

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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.
8 mins	2025-05-10 02:57:00.327Z	132.75° SE	2025-05-10 03:01:00.327Z	191.006° SSW	28.747°	2025-05-10 03:05:00.327Z	258.204° W
7 mins	2025-05-10 23:03:00.327Z	109.622° ESE	2025-05-10 23:06:00.327Z	167.595° S	28.704°	2025-05-10 23:10:00.327Z	227.058° WSW
7 mins	2025-05-11 00:37:00.327Z	105.84° ESE	2025-05-11 00:40:00.327Z	165.445° S	37.608°	2025-05-11 00:44:00.327Z	248.376° W

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.