OPS 4682 DEB, 38448

Orbit data source: Space-Track

OPS 4682 DEB, 38448 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 URL

https://www.satcat.com/sats-embedded/38448?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

38448, 1965-027FD

Orbit

LEO

Country

Related business

United States Air Force (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1965-04-03 (61 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: 17 hours ago

TLE from 17 hours ago

0 OPS 4682 DEB
1 38448U 65027FD  26121.11682258  .00000764  00000-0  24970-2 0  9993
2 38448  90.2418   5.6621 0031380   9.4153 350.7551 13.00310863548244

Epoch: 2026-05-01T02:48Z

TLE epoch observation values (Epoch: 2026-05-01T02:48:13.470Z)

Latitude

-0.00004°

Longitude

104.55229°

Altitude

1,240.091 km

Speed

7.246 km/s

True Right ascension

00h 22m 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

03:52:28

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,281.958 km

Perigee altitude

1,234.033 km

Semi-major axis

7,636.132 km

Eccentricity

0.00314

Inclination

90.2418°

RAAN

5.6621°

Arg. of periapsis

9.4153°

True anomaly

350.69711°

Mean anomaly

350.7551°

Eccentric anomaly

350.72613°

Mean motion

3.25262 °/min

Orbital period

110.68 mins

BSTAR

0.002497

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

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OPS 4682 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.
12 mins	2026-05-02 03:25:52.598Z	27.118° NE	2026-05-02 03:31:52.598Z	86.893° E	26.549°	2026-05-02 03:37:52.598Z	140.256° SSE
12 mins	2026-05-02 05:16:52.598Z	346.582° N	2026-05-02 05:21:52.598Z	288.25° WNW	37.64°	2026-05-02 05:28:52.598Z	208.863° SW
12 mins	2026-05-02 15:50:52.598Z	146.414° SSE	2026-05-02 15:56:52.598Z	78.047° E	35.992°	2026-05-02 16:02:52.598Z	12.134° NNE
11 mins	2026-05-02 17:42:52.598Z	226.87° WSW	2026-05-02 17:47:52.598Z	283.745° WNW	27.547°	2026-05-02 17:53:52.598Z	338.018° N

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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 OPS 4682 DEB, 38448 on other resources

View OPS 4682 DEB, 38448 on Heavens-Above

View OPS 4682 DEB, 38448 on Keep Track

View OPS 4682 DEB, 38448 on Celestrak

View OPS 4682 DEB, 38448 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

OPS 4682 DEB, 38448

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 17 hours ago

TLE from 17 hours ago

TLE epoch observation values (Epoch: 2026-05-01T02:48:13.470Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

OPS 4682 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out OPS 4682 DEB, 38448 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 17 hours ago