DECAYED

DELTA 1 R/B(2), 11984 (Decayed)

Orbit data source: Space-Track

DELTA 1 R/B(2), 11984 was space debris in LEO originally from a launch on Thu, 23 Mar 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.

Not visible in the next 10 days

Iframe embed code

<iframe src="https://www.satcat.com/sats-embedded/11984?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/11984?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

11984, 1967-026C

Orbit

Decayed

Last TLE update

2 weeks ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

UTC

Mission

Decayed spacecraft

Bus & Motor

FW4, Unknown motor

Mass

35 kg wet, 35 kg dry

Launch date (UTC)

1967-03-23 (58 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 1.5 m

Radar Cross Section

0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 2 weeks ago

0 DELTA 1 R/B(2)
1 11984U 67026C   25172.37959643  .11680063 -10374-4  18409-2 0  9996
2 11984  25.9592 214.8220 0136219 359.1556   0.8769 16.12067744557063

Epoch: 2025-06-21T09:06Z

TLE epoch observation values (Epoch: 2025-06-21T09:06:37.131Z)

Latitude

-0.00003°

Longitude

168.34781°

Altitude

149.008 km

Speed

7.873 km/s

True Right ascension

14h 19m 17s

True Declination

0° 00' 00"

Sunlit

Object was in full shadow at epoch

Visualization orbit readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

336.158 km

Perigee altitude

155.694 km

Semi-major axis

6,624.063 km

Eccentricity

0.01362

Inclination

25.9592°

RAAN

214.822°

Arg. of periapsis

359.1556°

True anomaly

Unknown

Mean anomaly

0.8769°

Eccentric anomaly

Unknown

Mean motion

4.02584 °/min

Orbital period

89.42 mins

BSTAR

0.0018409

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Other satellites on launch #26 in the year 1967 (1967-03-23 UTC)

INTELSAT 2-F3, 2717

DELTA 1 R/B(1), 2719 (Decayed)

DELTA 1 R/B(2) Visibility

Observer location: undefined°, undefined°

This satellite is decayed

Authenticating...

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Check out DELTA 1 R/B(2), 11984 (Decayed) on other resources

View DELTA 1 R/B(2), 11984 (Decayed) on Celestrak

View DELTA 1 R/B(2), 11984 (Decayed) on Gunter's Space Page

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