**DELTA 1 R/B(2) *, 2971**

Orbit data source: Space-Track

DELTA 1 R/B(2) *, 2971 is space debris in HEO originally from a launch on Thu, 28 Sep 1967 UTC launched from the Air Force Eastern Test Range (AFETR). 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/2971?theme=dark&initialShowStats=false

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Identifier

2971, 1967-094C

Orbit

HEO

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

UTC

Mission

Spacecraft

Bus & Motor

FW4, Unknown motor

Mass

~40 kg wet, ~40 kg dry

Launch date (UTC)

1967-09-28 (59 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 11 hours ago

TLE from 11 hours ago

0 DELTA 1 R/B(2) *
1 02971U 67094C   26127.15175173  .00003742  00000-0  13335-2 0  9996
2 02971  28.0310 201.6186 6551612  79.3724 343.3704  3.22522724558503

Epoch: 2026-05-07T03:38Z

TLE epoch observation values (Epoch: 2026-05-07T03:38:31.349Z)

Latitude

0.00004°

Longitude

-77.95629°

Altitude

3,463.656 km

Speed

7.772 km/s

True Right ascension

13h 26m 42s

True Declination

0° 00' 00"

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

23:00:34

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

25,656.127 km

Perigee altitude

295.93 km

Semi-major axis

19,354.165 km

Eccentricity

0.65516

Inclination

28.031°

RAAN

201.6186°

Arg. of periapsis

79.3724°

True anomaly

280.60332°

Mean anomaly

343.3704°

Eccentric anomaly

318.49409°

Mean motion

0.80609 °/min

Orbital period

446.6 mins

BSTAR

0.0013335

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Other satellites on launch #94 in the year 1967 (1967-09-28 UTC)

INTELSAT 2-F4, 2969

DELTA 1 R/B(1), 2970 (Decayed)

DELTA 1 DEB, 2972 (Decayed)

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DELTA 1 R/B(2) * 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.
255 mins	2026-05-07 19:22:10.830Z	225.056° WSW	2026-05-07 19:51:10.830Z	195.603° SSW	16.223°	2026-05-07 23:37:10.830Z	178.918° S

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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 R/B(2) *, 2971 on other resources

View DELTA 1 R/B(2) *, 2971 on Heavens-Above

View DELTA 1 R/B(2) *, 2971 on Keep Track

View DELTA 1 R/B(2) *, 2971 on Celestrak

View DELTA 1 R/B(2) *, 2971 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 R/B(2) *, 2971

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 11 hours ago

TLE from 11 hours ago

TLE epoch observation values (Epoch: 2026-05-07T03:38:31.349Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #94 in the year 1967 (1967-09-28 UTC)

DELTA 1 R/B(2) * Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 1 R/B(2) *, 2971 on other resources

Documentation

**DELTA 1 R/B(2) *, 2971**

Expand to show TLE details & history
Last TLE update: 11 hours ago