DELTA 1 R/B(2), 1318

Orbit data source: Space-Track

DELTA 1 R/B(2), 1318 is space debris in HEO originally from a launch on Tue, 06 Apr 1965 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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https://www.satcat.com/sats-embedded/1318?theme=dark&initialShowStats=false

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Identifier

1318, 1965-028B

Orbit

HEO

Last TLE update

3 days ago

Origin

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

ABL

Mission

Spacecraft

Bus & Motor

ALTAIR, Unknown motor

Mass

33 kg wet, 33 kg dry

Launch date (UTC)

1965-04-06 (60 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 3 days ago

0 DELTA 1 R/B(2)
1 01318U 65028B   25106.44028082 -.00000100  00000-0  00000-0 0  9998
2 01318  18.2183  22.1525 6939572 295.1239 209.2653  2.11824462 98281

Epoch: 2025-04-16T10:34Z

Definitive object data (Epoch: 2025-04-16T10:34:00.262Z)

Latitude

15.27623°

Longitude

142.79047°

Altitude

36,167.164 km

Speed

1.782 km/s

True Right ascension

09h 44m 28s

True Declination

15° 15' 42"

Sunlit

Object was in daylight at TLE epoch

Visualization TLE readout

Latitude

3.9743°

Longitude

-174.30864°

Altitude

17,517.497 km

Speed

4.219 km/s

Apparent Right ascension

13h 08m 55s

Apparent Declination

-5° 05' 42"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

04:05:03

Azimuth

60.52° ENE

Elevation

-37.316°

Doppler factor

Orbital elements

Apogee altitude

37,011.612 km

Perigee altitude

1,460.975 km

Semi-major axis

25,614.431 km

Eccentricity

0.6939572

Inclination

18.2183°

RAAN

22.1525°

Arg. of periapsis

295.1239°

True anomaly

187.43629°

Mean anomaly

209.2653°

Eccentric anomaly

197.38508°

Mean motion

0.52944 °/min

BSTAR

Unknown

Orbital period

679.96 mins

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Other satellites on launch #28 in the year 1965 (1965-04-06 UTC)

INTELSAT 1-F1, 1317

DELTA 1 R/B(2) 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.
615 mins	2025-04-19 23:10:38.909Z	243.031° WSW	2025-04-20 01:26:38.909Z	210.743° SW	41.051°	2025-04-20 09:25:38.909Z	200.594° SSW

Authenticating...

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Check out DELTA 1 R/B(2), 1318 on other resources

View DELTA 1 R/B(2), 1318 on Heavens-Above

View DELTA 1 R/B(2), 1318 on Keep Track

View DELTA 1 R/B(2), 1318 on Celestrak

View DELTA 1 R/B(2), 1318 on Gunter's Space Page

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