DELTA 1 R/B, 862

Orbit data source: Space-Track

DELTA 1 R/B, 862 is space debris in HEO originally from a launch on Wed, 19 Aug 1964 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 src="https://www.satcat.com/sats-embedded/862?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/862?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

862, 1964-047B

Orbit

HEO

Last TLE update

1 day ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

ABL

Mission

Spacecraft

Bus & Motor

ALTAIR, Unknown motor

Mass

~38 kg wet, ~38 kg dry

Launch date (UTC)

1964-08-19 (61 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 1 day ago

0 DELTA 1 R/B
1 00862U 64047B   25128.02193282 -.00000174  00000-0  00000-0 0  9995
2 00862  16.2687  86.1535 7134014 173.0347 209.0468  2.05102621249846

Epoch: 2025-05-08T00:31Z

Definitive object data (Epoch: 2025-05-08T00:31:34.995Z)

Latitude

-0.00006°

Longitude

-147.8463°

Altitude

37,631.715 km

Speed

1.698 km/s

True Right ascension

05h 44m 35s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-15.15392°

Longitude

143.64474°

Altitude

12,748.377 km

Speed

5.143 km/s

Apparent Right ascension

01h 20m 15s

Apparent Declination

-21° 15' 46"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

13:56:58

Azimuth

25.46° NE

Elevation

-69.772°

Doppler factor

Orbital elements

Apogee altitude

38,463.904 km

Perigee altitude

1,122.538 km

Semi-major axis

26,171.358 km

Eccentricity

0.7134014

Inclination

16.2687°

RAAN

86.1535°

Arg. of periapsis

173.0347°

True anomaly

187.01931°

Mean anomaly

209.0468°

Eccentric anomaly

197.05715°

Mean motion

0.51263 °/min

BSTAR

Unknown

Orbital period

702.26 mins

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Other satellites on launch #47 in the year 1964 (1964-08-19 UTC)

SYNCOM 3, 858

DELTA 1 R/B Visibility forecast

Observer location: undefined°, undefined°

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.
642 mins	2025-05-09 17:18:14.205Z	196.263° SSW	2025-05-10 03:43:14.205Z	201.659° SSW	34.73°	2025-05-10 04:00:14.205Z	133.567° SE

Authenticating...

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Check out DELTA 1 R/B, 862 on other resources

View DELTA 1 R/B, 862 on Heavens-Above

View DELTA 1 R/B, 862 on Keep Track

View DELTA 1 R/B, 862 on Celestrak

View DELTA 1 R/B, 862 on Gunter's Space Page

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