DELTA 1 DEB, 2976

Orbit data source: Space-Track

DELTA 1 DEB, 2976 is space debris in SSO originally from a launch on Thu, 20 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 URL

https://www.satcat.com/sats-embedded/2976?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

2976, 1967-036C

Orbit

SSO

Country

Related business

National Oceanic and Atmospheric Administration (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1967-04-20 (59 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: 5 days ago

TLE from 5 days ago

0 DELTA 1 DEB
1 02976U 67036C   25335.32848514 -.00000033  00000-0  75242-4 0  9990
2 02976 102.1460 111.5825 0098588 153.7521 235.6972 12.82097089742356

Epoch: 2025-12-01T07:53Z

TLE epoch observation values (Epoch: 2025-12-01T07:53:01.116Z)

Latitude

27.86921°

Longitude

-83.60396°

Altitude

1,379.556 km

Speed

7.152 km/s

True Right ascension

07h 00m 19s

True Declination

27° 44' 19"

Sunlit

Object was in full shadow 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

19:07:51

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

1,406.577 km

Perigee altitude

1,254.58 km

Semi-major axis

7,708.715 km

Eccentricity

0.00986

Inclination

102.146°

RAAN

111.5825°

Arg. of periapsis

153.7521°

True anomaly

234.77044°

Mean anomaly

235.6972°

Eccentric anomaly

235.23317°

Mean motion

3.20679 °/min

Orbital period

112.26 mins

BSTAR

0.000075242

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Other satellites on launch #36 in the year 1967 (1967-04-20 UTC)

DELTA 1 DEB, 2977

DELTA 1 R/B, 2758

ESSA 5, 2757

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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.
12 mins	2025-12-05 22:50:39.733Z	7.536° NNE	2025-12-05 22:55:39.733Z	311.376° NW	40.833°	2025-12-05 23:02:39.733Z	217.079° SW
12 mins	2025-12-06 07:44:39.733Z	112.497° ESE	2025-12-06 07:50:39.733Z	52.453° ENE	28.052°	2025-12-06 07:56:39.733Z	0.335° NNE
13 mins	2025-12-06 09:33:39.733Z	181.898° SSW	2025-12-06 09:39:39.733Z	244.245° WSW	39.563°	2025-12-06 09:46:39.733Z	331.278° NNW

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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, 2976 on other resources

View DELTA 1 DEB, 2976 on Heavens-Above

View DELTA 1 DEB, 2976 on Keep Track

View DELTA 1 DEB, 2976 on Celestrak

View DELTA 1 DEB, 2976 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, 2976

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 5 days ago

TLE from 5 days ago

TLE epoch observation values (Epoch: 2025-12-01T07:53:01.116Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #36 in the year 1967 (1967-04-20 UTC)

DELTA 1 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 1 DEB, 2976 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 5 days ago