**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.

Loading next visibility...

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/2971?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/2971?theme=dark&initialShowStats=false

Optional Secondary NORAD IDs

Max 10 NORAD IDs; Separated by commas

Initial load time (optional)

ISO8601 Format

TLE date request (optional)

ISO8601 Format

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 (58 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: 3 days ago

TLE from 3 days ago

0 DELTA 1 R/B(2) *
1 02971U 67094C   25310.11720998  .00009508  00000-0  45168-2 0  9991
2 02971  28.3677 302.3561 6555282 274.9126  18.6124  3.20923932552645

Epoch: 2025-11-06T02:48Z

TLE epoch observation values (Epoch: 2025-11-06T02:48:46.942Z)

Latitude

-0.00037°

Longitude

-145.47656°

Altitude

4,085.751 km

Speed

7.46 km/s

True Right ascension

20h 09m 11s

True Declination

0° 00' 01"

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

05:28:44

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

25,769.463 km

Perigee altitude

310.932 km

Semi-major axis

19,418.334 km

Eccentricity

0.65553

Inclination

28.3677°

RAAN

302.3561°

Arg. of periapsis

274.9126°

True anomaly

84.92839°

Mean anomaly

18.6124°

Eccentric anomaly

45.31729°

Mean motion

0.80209 °/min

Orbital period

448.83 mins

BSTAR

0.0045168

Loading maneuver chart data...

Computing Atmospheric mass density...

Loading historical data...

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)

Did you know?

You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

Click here to try in Sandbox

DELTA 1 R/B(2) * Visibility forecast

Loading observer location...
Set Observer location

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.
182 mins	2025-11-09 09:14:01.165Z	260.847° W	2025-11-09 09:14:01.165Z	260.847° W	36.886°	2025-11-09 12:16:01.165Z	178.313° S
300 mins	2025-11-10 04:14:01.165Z	248.117° W	2025-11-10 07:00:01.165Z	232.069° WSW	42.976°	2025-11-10 09:14:01.165Z	214.932° SW

Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

Please sign-in to view Co-orbital & Co-planar RSOs.

Click to sort rows by RSO header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Type header in ascending order	Click to sort rows by Inclination Δ header in ascending order	Click to sort rows by RAAN Δ header in ascending order	Click to sort rows by Coplanar Angle header in ascending order	Click to sort rows by SMA Δ header in ascending order	Click to sort rows by Orbital period header in ascending order	Click to sort rows by <5km Md TCA header in ascending order

CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

Authenticating...

Click to sort rows by Secondary header in ascending order	Click to sort rows by Secondary name header in ascending order	Click to sort rows by Country header in ascending order	Click to sort rows by Owner header in ascending order	Click to sort rows by Obj. Type header in ascending order	Click to sort rows by Miss dist. header in ascending order	Click to sort rows by Rel. speed header in ascending order	Click to sort rows by Apr. angle header in ascending order	Click to sort rows by TCA header in ascending order

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: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2025-11-06T02:48:46.942Z)

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: 3 days ago