OPS 4682 DEB, 38449

Orbit data source: Space-Track

OPS 4682 DEB, 38449 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/38449?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

38449, 1965-027FE

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: 15 hours ago

TLE from 15 hours ago

0 OPS 4682 DEB
1 38449U 65027FE  26119.14180718  .00000381  00000-0  13287-2 0  9992
2 38449  90.2481   9.8983 0030438 300.7571  59.0552 12.95257077581287

Epoch: 2026-04-29T03:24Z

TLE epoch observation values (Epoch: 2026-04-29T03:24:12.140Z)

Latitude

-0.00001°

Longitude

101.7407°

Altitude

1,271.666 km

Speed

7.225 km/s

True Right ascension

00h 39m 35s

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

01:44:57

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,301.164 km

Perigee altitude

1,254.557 km

Semi-major axis

7,655.997 km

Eccentricity

0.00304

Inclination

90.2481°

RAAN

9.8983°

Arg. of periapsis

300.7571°

True anomaly

59.35493°

Mean anomaly

59.0552°

Eccentric anomaly

59.20501°

Mean motion

3.23997 °/min

Orbital period

111.11 mins

BSTAR

0.0013287

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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	2026-04-29 18:20:33.448Z	224.297° SW	2026-04-29 18:26:33.448Z	278.419° WNW	24.804°	2026-04-29 18:32:33.448Z	333.328° NNW
13 mins	2026-04-30 04:07:33.448Z	21.162° NNE	2026-04-30 04:13:33.448Z	83.575° E	32.726°	2026-04-30 04:20:33.448Z	151.782° SSE
12 mins	2026-04-30 05:58:33.448Z	343.458° N	2026-04-30 06:04:33.448Z	280.586° WNW	32.27°	2026-04-30 06:10:33.448Z	220.94° SW
13 mins	2026-04-30 16:35:33.448Z	158.809° S	2026-04-30 16:41:33.448Z	74.973° E	42.03°	2026-04-30 16:48:33.448Z	4.175° NNE

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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, 38449 on other resources

View OPS 4682 DEB, 38449 on Heavens-Above

View OPS 4682 DEB, 38449 on Keep Track

View OPS 4682 DEB, 38449 on Celestrak

View OPS 4682 DEB, 38449 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, 38449

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 15 hours ago

TLE from 15 hours ago

TLE epoch observation values (Epoch: 2026-04-29T03:24:12.140Z)

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, 38449 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 15 hours ago