**OPS 0100 DEB *, 4843**

Orbit data source: Space-Track

OPS 0100 DEB *, 4843 is space debris in LEO originally from a launch on Fri, 14 Apr 1967 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/4843?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/4843?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

4843, 1967-034E

Orbit

LEO

Last TLE update

17 hours ago

Origin

United States Navy (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1967-04-14 (58 years ago)

Launch vehicle

Unknown

Launch site

Air Force Western Test Range (AFWTR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 17 hours ago

0 OPS 0100 DEB *
1 04843U 67034E   25199.26530005  .00000143  00000-0  20314-3 0  9997
2 04843  90.3797 128.7917 0028761  25.9930 126.9920 13.52552387228500

Epoch: 2025-07-18T06:22Z

TLE epoch observation values (Epoch: 2025-07-18T06:22:01.924Z)

Latitude

26.78558°

Longitude

-82.84486°

Altitude

1,079.126 km

Speed

7.308 km/s

True Right ascension

20h 35m 55s

True Declination

26° 39' 12"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

Latitude

28.46502°

Longitude

96.7871°

Altitude

1,045.114 km

Speed

7.342 km/s

Apparent Right ascension

05h 26m 29s

Apparent Declination

-5° 40' 13"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

12:18:04

Azimuth

273.935° WNW

Elevation

-13.517°

Doppler factor

Orbital elements

Apogee altitude

1,081.322 km

Perigee altitude

1,038.536 km

Semi-major axis

7,438.066 km

Eccentricity

0.00288

Inclination

90.3797°

RAAN

128.7917°

Arg. of periapsis

25.993°

True anomaly

127.25467°

Mean anomaly

126.992°

Eccentric anomaly

127.12339°

Mean motion

3.3834 °/min

Orbital period

106.4 mins

BSTAR

0.00020314

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Other satellites on launch #34 in the year 1967 (1967-04-14 UTC)

OPS 0100 (TRANSIT 15), 2754

SCOUT A R/B, 2755

SCOUT A DEB, 2777

SCOUT A DEB, 2778

SCOUT A DEB, 6718 (Decayed)

TRANSIT 15 DEB, 7670 (Decayed)

TRANSIT 15 DEB, 22172 (Decayed)

TRANSIT 15 DEB, 29180 (Decayed)

TRANSIT 15 DEB, 29265 (Decayed)

TRANSIT 15 DEB, 29276 (Decayed)

OPS 0100 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.
12 mins	2025-07-19 07:03:27.237Z	15.331° NNE	2025-07-19 07:09:27.237Z	84.894° E	36.097°	2025-07-19 07:15:27.237Z	158.985° S
9 mins	2025-07-19 08:51:27.237Z	331.307° NNW	2025-07-19 08:55:27.237Z	284.571° WNW	25.027°	2025-07-19 09:00:27.237Z	231.686° WSW
10 mins	2025-07-19 19:01:27.237Z	144.965° SSE	2025-07-19 19:05:27.237Z	92.178° ESE	35.767°	2025-07-19 19:11:27.237Z	11.157° NNE
9 mins	2025-07-19 20:48:27.237Z	231.684° WSW	2025-07-19 20:52:27.237Z	279.671° WNW	24.014°	2025-07-19 20:57:27.237Z	332.133° NNW

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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Check out OPS 0100 DEB *, 4843 on other resources

View OPS 0100 DEB *, 4843 on Heavens-Above

View OPS 0100 DEB *, 4843 on Keep Track

View OPS 0100 DEB *, 4843 on Celestrak

View OPS 0100 DEB *, 4843 on Gunter's Space Page

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