OPS 4682 DEB, 1389

Orbit data source: Space-Track

OPS 4682 DEB, 1389 is space debris in LEO originally from a launch on Sat, 03 Apr 1965 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 src="https://www.satcat.com/sats-embedded/1389?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/1389?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

1389, 1965-027D

Orbit

LEO

Last TLE update

11 hours ago

Origin

United States Space Force (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

7 kg wet, 7 kg dry

Launch date (UTC)

1965-04-03 (60 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Half Cyl, 2 m

Radar Cross Section

2.370 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 11 hours ago

0 OPS 4682 DEB
1 01389U 65027D   25151.75852991  .00000864  00000-0  23117-2 0  9995
2 01389  89.8459 224.8167 0030951 109.4866  12.3148 13.14177650860578

Epoch: 2025-05-31T18:12Z

TLE epoch observation values (Epoch: 2025-05-31T18:12:16.984Z)

Latitude

58.21274°

Longitude

-117.99579°

Altitude

1,193.987 km

Speed

7.273 km/s

True Right ascension

02h 58m 16s

True Declination

58° 04' 03"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

40.20528°

Longitude

-117.88469°

Altitude

1,192.788 km

Speed

7.271 km/s

Apparent Right ascension

02h 56m 57s

Apparent Declination

4° 15' 07"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

14:54:52

Azimuth

359.254° N

Elevation

-45.829°

Doppler factor

Orbital elements

Apogee altitude

1,227.612 km

Perigee altitude

1,180.676 km

Semi-major axis

7,582.281 km

Eccentricity

0.0031

Inclination

89.8459°

RAAN

224.8167°

Arg. of periapsis

109.4866°

True anomaly

Unknown

Mean anomaly

12.3148°

Eccentric anomaly

Unknown

Mean motion

3.28733 °/min

Orbital period

109.51 mins

BSTAR

0.0023117

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Other satellites on launch #27 in the year 1965 (1965-04-03 UTC)

OPS 4682 (SNAPSHOT), 1314

OPS 4682 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.
11 mins	2025-06-01 06:29:33.170Z	225.137° WSW	2025-06-01 06:35:33.170Z	284.656° WNW	24.521°	2025-06-01 06:40:33.170Z	332.268° NNW
11 mins	2025-06-01 16:08:33.170Z	29.295° NE	2025-06-01 16:13:33.170Z	86.641° E	28.036°	2025-06-01 16:19:33.170Z	143.956° SSE
11 mins	2025-06-01 17:57:33.170Z	343.653° N	2025-06-01 18:02:33.170Z	284.991° WNW	34.651°	2025-06-01 18:08:33.170Z	214.736° SW
11 mins	2025-06-02 04:25:33.170Z	143.109° SSE	2025-06-02 04:30:33.170Z	86.193° E	34.627°	2025-06-02 04:36:33.170Z	14.481° NNE

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Check out OPS 4682 DEB, 1389 on other resources

View OPS 4682 DEB, 1389 on Heavens-Above

View OPS 4682 DEB, 1389 on Keep Track

View OPS 4682 DEB, 1389 on Celestrak

View OPS 4682 DEB, 1389 on Gunter's Space Page

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