DELTA 1 DEB, 3127

Orbit data source: Space-Track

DELTA 1 DEB, 3127 is space debris in LEO originally from a launch on Thu, 11 Jan 1968 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/3127?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

3127, 1968-002D

Orbit

LEO

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1968-01-11 (58 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: 8 hours ago

TLE from 8 hours ago

0 DELTA 1 DEB
1  3127U 68002D   26083.52838346 -.00000044  00000-0  88682-4 0  9992
2  3127 105.3094 201.1351 0320646  87.3083 342.2993 12.84891751728094

Epoch: 2026-03-24T12:40Z

TLE epoch observation values (Epoch: 2026-03-24T12:40:52.330Z)

Latitude

63.87135°

Longitude

155.1879°

Altitude

1,098.048 km

Speed

7.42 km/s

True Right ascension

11h 09m 38s

True Declination

63° 44' 29"

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

01:53:55

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,566.43 km

Perigee altitude

1,072.78 km

Semi-major axis

7,697.742 km

Eccentricity

0.03206

Inclination

105.3094°

RAAN

201.1351°

Arg. of periapsis

87.3083°

True anomaly

341.13794°

Mean anomaly

342.2993°

Eccentric anomaly

341.72315°

Mean motion

3.21365 °/min

Orbital period

112.02 mins

BSTAR

0.000088682

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Other satellites on launch #2 in the year 1968 (1968-01-11 UTC)

EXPLORER 36 (GEOS 2), 3093

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DELTA 1 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.
11 mins	2026-03-24 22:15:03.241Z	0.083° NNE	2026-03-24 22:20:03.241Z	304.206° NW	27.98°	2026-03-24 22:26:03.241Z	244.452° WSW
4 mins	2026-03-25 05:24:03.241Z	62.598° ENE	2026-03-25 05:26:03.241Z	42.502° NE	14.391°	2026-03-25 05:28:03.241Z	23.086° NE
11 mins	2026-03-25 07:09:03.241Z	148.364° SSE	2026-03-25 07:14:03.241Z	92.08° ESE	44.098°	2026-03-25 07:20:03.241Z	341.656° N
7 mins	2026-03-25 09:01:03.241Z	227.382° WSW	2026-03-25 09:04:03.241Z	255.443° W	16.841°	2026-03-25 09:08:03.241Z	295.042° NW

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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 DELTA 1 DEB, 3127 on other resources

View DELTA 1 DEB, 3127 on Heavens-Above

View DELTA 1 DEB, 3127 on Keep Track

View DELTA 1 DEB, 3127 on Celestrak

View DELTA 1 DEB, 3127 on Gunter's Space Page

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

DELTA 1 DEB, 3127

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 8 hours ago

TLE from 8 hours ago

TLE epoch observation values (Epoch: 2026-03-24T12:40:52.330Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #2 in the year 1968 (1968-01-11 UTC)

DELTA 1 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 1 DEB, 3127 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 8 hours ago