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

5 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 5 days ago

0 DELTA 1 R/B
1 00862U 64047B   25180.04502758 -.00000185  00000-0  00000-0 0  9999
2 00862  16.5398  71.3382 7128105 200.9070 100.8542  2.05100604250911

Epoch: 2025-06-29T01:04Z

TLE epoch observation values (Epoch: 2025-06-29T01:04:50.382Z)

Latitude

0.00009°

Longitude

137.79687°

Altitude

32,152.963 km

Speed

2.336 km/s

True Right ascension

04h 45m 31s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

8.61863°

Longitude

166.93028°

Altitude

37,375.272 km

Speed

1.729 km/s

Apparent Right ascension

06h 17m 30s

Apparent Declination

3° 10' 50"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

13:34:11

Azimuth

285.017° WNW

Elevation

-12.47°

Doppler factor

Orbital elements

Apogee altitude

38,448.682 km

Perigee altitude

1,138.043 km

Semi-major axis

26,171.5 km

Eccentricity

0.71281

Inclination

16.5398°

RAAN

71.3382°

Arg. of periapsis

200.907°

True anomaly

Unknown

Mean anomaly

100.8542°

Eccentric anomaly

Unknown

Mean motion

0.51263 °/min

Orbital period

702.27 mins

BSTAR

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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.
133 mins	2025-07-04 14:29:20.952Z	91.954° ESE	2025-07-04 15:50:20.952Z	93.255° ESE	14.01°	2025-07-04 16:42:20.952Z	89.904° E

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.