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

Optional Secondary NORAD IDs

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ISO8601 Format

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ISO8601 Format

Identifier

1389, 1965-027D

Orbit

LEO

Last TLE update

20 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 20 hours ago

0 OPS 4682 DEB
1 01389U 65027D   25185.87890387  .00000425  00000-0  11258-2 0  9992
2 01389  89.8467 224.3251 0025536  23.1076 153.4872 13.14215728865052

Epoch: 2025-07-04T21:05Z

TLE epoch observation values (Epoch: 2025-07-04T21:05:37.294Z)

Latitude

3.18066°

Longitude

164.78626°

Altitude

1,226.785 km

Speed

7.233 km/s

True Right ascension

02h 57m 15s

True Declination

3° 09' 46"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

67.31892°

Longitude

164.41781°

Altitude

1,219.206 km

Speed

7.251 km/s

Apparent Right ascension

18h 50m 34s

Apparent Declination

47° 24' 03"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

04:47:20

Azimuth

339.707° N

Elevation

1.516°

Doppler factor

Orbital elements

Apogee altitude

1,223.359 km

Perigee altitude

1,184.635 km

Semi-major axis

7,582.134 km

Eccentricity

0.00255

Inclination

89.8467°

RAAN

224.3251°

Arg. of periapsis

23.1076°

True anomaly

Unknown

Mean anomaly

153.4872°

Eccentric anomaly

Unknown

Mean motion

3.28743 °/min

Orbital period

109.51 mins

BSTAR

0.0011258

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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.
5 mins	2025-07-05 16:56:03.862Z	315.987° NNW	2025-07-05 16:59:03.862Z	291.058° WNW	12.588°	2025-07-05 17:01:03.862Z	274.267° WNW
9 mins	2025-07-06 01:35:03.862Z	113.211° SE	2025-07-06 01:39:03.862Z	71.705° E	22.158°	2025-07-06 01:44:03.862Z	25.364° NE
12 mins	2025-07-06 03:22:03.862Z	195.395° SSW	2025-07-06 03:28:03.862Z	283.698° WNW	40.556°	2025-07-06 03:34:03.862Z	349.028° N
6 mins	2025-07-06 13:03:03.862Z	51.938° ENE	2025-07-06 13:06:03.862Z	78.165° E	13.856°	2025-07-06 13:09:03.862Z	103.204° ESE
13 mins	2025-07-06 14:50:03.862Z	2.751° NNE	2025-07-06 14:56:03.862Z	119.907° SE	44.975°	2025-07-06 15:03:03.862Z	183.029° SSW
6 mins	2025-07-06 16:42:03.862Z	311.672° NW	2025-07-06 16:44:03.862Z	293.553° NW	15.317°	2025-07-06 16:48:03.862Z	259.045° W

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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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