DELTA 1 R/B, 1983

Orbit data source: Space-Track

DELTA 1 R/B, 1983 is space debris in SSO originally from a launch on Thu, 03 Feb 1966 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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ISO8601 Format

Identifier

1983, 1966-008B

Orbit

SSO

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

ABL

Mission

Spacecraft

Bus & Motor

ALTAIR, Unknown motor

Mass

60 kg wet, 60 kg dry

Launch date (UTC)

1966-02-03 (60 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

Medium (>0.1 m² and <1 m²)

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Last TLE update: 9 hours ago

TLE from 9 hours ago

0 DELTA 1 R/B
1  1983U 66008B   26062.34596079  .00001777  00000-0  30570-3 0  9990
2  1983  98.0333 341.6840 0065257  71.2525 289.5746 14.68442766157105

Epoch: 2026-03-03T08:18Z

TLE epoch observation values (Epoch: 2026-03-03T08:18:11.012Z)

Latitude

-0.00007°

Longitude

56.01178°

Altitude

653.909 km

Speed

7.539 km/s

True Right ascension

22h 46m 44s

True Declination

0° 00' 00"

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

21:18:50

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

709.055 km

Perigee altitude

617.157 km

Semi-major axis

7,041.243 km

Eccentricity

0.00653

Inclination

98.0333°

RAAN

341.684°

Arg. of periapsis

71.2525°

True anomaly

288.86811°

Mean anomaly

289.5746°

Eccentric anomaly

289.22155°

Mean motion

3.67341 °/min

Orbital period

98 mins

BSTAR

0.0003057

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Other satellites on launch #8 in the year 1966 (1966-02-03 UTC)

DELTA 1 DEB, 2118

ESSA 1 (OT-3), 1982

DELTA 1 DEB, 2154

DELTA 1 DEB, 2085 (Decayed)

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DELTA 1 R/B 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.
7 mins	2026-03-03 18:14:16.932Z	150.312° SSE	2026-03-03 18:18:16.932Z	57.911° ENE	39.526°	2026-03-03 18:21:16.932Z	359.289° N
7 mins	2026-03-04 07:46:16.932Z	358.014° N	2026-03-04 07:49:16.932Z	285.284° WNW	39.257°	2026-03-04 07:53:16.932Z	210.522° SW

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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, 1983 on other resources

View DELTA 1 R/B, 1983 on Heavens-Above

View DELTA 1 R/B, 1983 on Keep Track

View DELTA 1 R/B, 1983 on Celestrak

View DELTA 1 R/B, 1983 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, 1983

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 9 hours ago

TLE from 9 hours ago

TLE epoch observation values (Epoch: 2026-03-03T08:18:11.012Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #8 in the year 1966 (1966-02-03 UTC)

DELTA 1 R/B Visibility forecast

Co-orbital & Co-planar RSOs

Check out DELTA 1 R/B, 1983 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 9 hours ago