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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Iframe URL

https://www.satcat.com/sats-embedded/1318?theme=dark&initialShowStats=false

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Identifier

1318, 1965-028B

Orbit

HEO

Country

Related business

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 (61 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: 2 days ago

TLE from 2 days ago

0 DELTA 1 R/B(2)
1 01318U 65028B   26162.18082337 -.00000149  00000-0  00000-0 0  9998
2 01318  17.7500 267.6102 6944015 147.9753 285.8018  2.11826754107202

Epoch: 2026-06-11T04:20Z

TLE epoch observation values (Epoch: 2026-06-11T04:20:23.139Z)

Latitude

0.09226°

Longitude

-56.76872°

Altitude

25,729.582 km

Speed

3.044 km/s

True Right ascension

17h 51m 25s

True Declination

0° 05' 32"

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

13:22:13

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

37,022.748 km

Perigee altitude

1,449.55 km

Semi-major axis

25,614.286 km

Eccentricity

0.6944

Inclination

17.75°

RAAN

267.6102°

Arg. of periapsis

147.9753°

True anomaly

212.3854°

Mean anomaly

285.8018°

Eccentric anomaly

248.72658°

Mean motion

0.52944 °/min

Orbital period

679.96 mins

BSTAR

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

INTELSAT 1-F1, 1317

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DELTA 1 R/B(2) 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.
24 mins	2026-06-13 14:49:55.396Z	255.838° W	2026-06-13 15:07:55.396Z	207.372° SW	22.158°	2026-06-13 15:13:55.396Z	161.088° S

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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(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.

DELTA 1 R/B(2), 1318

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-06-11T04:20:23.139Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

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

DELTA 1 R/B(2) Visibility forecast

Co-orbital & Co-planar RSOs

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

Documentation

Expand to show TLE details & history
Last TLE update: 2 days ago