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
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 DELTA 1 R/B
1 01729U 65089B   26135.22807591 -.00000081  00000-0 -37697-4 0  9995
2 01729  59.3899  87.2931 0713941 168.5594 304.2639 11.97573198646472
Epoch: 2026-05-15T05:28Z
TLE epoch observation values (Epoch: 2026-05-15T05:28:25.758Z)
Latitude
56.06532°
Longitude
-108.81214°
Altitude
1,405.11 km
Speed
7.293 km/s
True Right ascension
13h 45m 01s
True Declination
55° 55' 09"
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
19:11:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,267.237 km
Perigee altitude
1,115.039 km
Semi-major axis
8,069.275 km
Eccentricity
0.07139
Inclination
59.3899°
RAAN
87.2931°
Arg. of periapsis
168.5594°
True anomaly
297.16399°
Mean anomaly
304.2639°
Eccentric anomaly
300.74837°
Mean motion
2.99427 °/min
Orbital period
120.23 mins
BSTAR
-0.000037697
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