OV1-5 DEB, 5599

Orbit data source: Space-Track

OV1-5 DEB, 5599 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/5599?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

5599, 1966-025G

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: 11 hours ago

TLE from 11 hours ago

0 OV1-5 DEB
1  5599U 66025G   26077.64709271  .00028551  00000-0  23619-2 0  9999
2  5599 144.6113   0.9102 0022527 219.0241 140.8844 14.96939818 91039

Epoch: 2026-03-18T15:31Z

TLE epoch observation values (Epoch: 2026-03-18T15:31:48.810Z)

Latitude

0°

Longitude

-48.25104°

Altitude

587.485 km

Speed

7.562 km/s

True Right ascension

00h 03m 38s

True Declination

0° 00' 00"

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

07:25:18

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

595.184 km

Perigee altitude

563.837 km

Semi-major axis

6,957.648 km

Eccentricity

0.00225

Inclination

144.6113°

RAAN

0.9102°

Arg. of periapsis

219.0241°

True anomaly

141.0469°

Mean anomaly

140.8844°

Eccentric anomaly

140.96569°

Mean motion

3.73981 °/min

Orbital period

96.26 mins

BSTAR

0.0023619

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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)

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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.
5 mins	2026-03-19 11:13:07.186Z	114.449° SE	2026-03-19 11:15:07.186Z	151.06° SSE	21.798°	2026-03-19 11:18:07.186Z	210.113° SW
5 mins	2026-03-19 12:45:07.186Z	116.783° SE	2026-03-19 12:47:07.186Z	177.478° S	33.802°	2026-03-19 12:50:07.186Z	241.301° WSW
6 mins	2026-03-19 14:16:07.186Z	123.218° SE	2026-03-19 14:18:07.186Z	171.91° S	34.184°	2026-03-19 14:22:07.186Z	258.009° W
5 mins	2026-03-19 15:48:07.186Z	157.917° S	2026-03-19 15:50:07.186Z	203.847° SW	23.89°	2026-03-19 15:53:07.186Z	254.68° 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, 5599 on other resources

View OV1-5 DEB, 5599 on Heavens-Above

View OV1-5 DEB, 5599 on Keep Track

View OV1-5 DEB, 5599 on Celestrak

View OV1-5 DEB, 5599 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, 5599

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2026-03-18T15:31:48.810Z)

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, 5599 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 11 hours ago