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

2 days 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 2 days ago

0 DELTA 1 R/B
1 00862U 64047B   25118.29844841 -.00000059  00000-0  00000-0 0  9999
2 00862  16.2111  88.9574 7134230 167.7915 229.6187  2.05100615249647

Epoch: 2025-04-28T07:09Z

Definitive object data (Epoch: 2025-04-28T07:09:45.942Z)

Latitude

-0.00022°

Longitude

125.01406°

Altitude

36,024.902 km

Speed

1.889 km/s

True Right ascension

05h 55m 52s

True Declination

0° 00' 01"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

-9.2823°

Longitude

90.24658°

Altitude

30,523.859 km

Speed

2.524 km/s

Apparent Right ascension

03h 05m 53s

Apparent Declination

-15° 33' 12"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

09:01:09

Azimuth

257.222° W

Elevation

-9.019°

Doppler factor

Orbital elements

Apogee altitude

38,464.77 km

Perigee altitude

1,122.022 km

Semi-major axis

26,171.533 km

Eccentricity

0.713423

Inclination

16.2111°

RAAN

88.9574°

Arg. of periapsis

167.7915°

True anomaly

192.28838°

Mean anomaly

229.6187°

Eccentric anomaly

209.49404°

Mean motion

0.51262 °/min

BSTAR

Unknown

Orbital period

702.27 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.
137 mins	2025-04-30 18:18:37.056Z	104.168° ESE	2025-04-30 19:43:37.056Z	104.678° ESE	14.477°	2025-04-30 20:35:37.056Z	98.324° ESE

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.