DELTA 1 R/B, 1729

Orbit data source: Space-Track

DELTA 1 R/B, 1729 is space debris in LEO originally from a launch on Sat, 06 Nov 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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Identifier
1729, 1965-089B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
~60 kg wet, ~60 kg dry
Launch date (UTC)
1965-11-06 (61 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago
0 DELTA 1 R/B
1 01729U 65089B   26279.07431896 -.00000065  00000-0  47303-4 0  9994
2 01729  59.3924 123.7808 0708835 262.6797 185.3921 11.97579308663703
Epoch: 2026-10-06T01:47Z
TLE epoch observation values (Epoch: 2026-10-06T01:47:01.158Z)
Latitude
59.40195°
Longitude
167.1224°
Altitude
2,270.201 km
Speed
6.551 km/s
True Right ascension
13h 54m 29s
True Declination
59° 16' 39"
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
13:23:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,263.087 km
Perigee altitude
1,119.134 km
Semi-major axis
8,069.247 km
Eccentricity
0.07088
Inclination
59.3924°
RAAN
123.7808°
Arg. of periapsis
262.6797°
True anomaly
184.69087°
Mean anomaly
185.3921°
Eccentric anomaly
185.03562°
Mean motion
2.99429 °/min
Orbital period
120.23 mins
BSTAR
0.000047303
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