DELTA 1 R/B, 3036

Orbit data source: Space-Track

DELTA 1 R/B, 3036 is space debris in SSO originally from a launch on Fri, 10 Nov 1967 UTC launched from the Air Force Western Test Range (AFWTR). 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
3036, 1967-114B
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
UTC
Mission
Spacecraft
Bus & Motor
FW4, Unknown motor
Mass
~40 kg wet, ~40 kg dry
Launch date (UTC)
1967-11-10 (58 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.8 m
Radar Cross Section
0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 10 hours ago

TLE from 10 hours ago
0 DELTA 1 R/B
1 03036U 67114B   25258.48215782 -.00000044  00000-0  18149-4 0  9996
2 03036 102.0142 351.1072 0047746 303.1806  67.8696 12.54133479647910
Epoch: 2025-09-15T11:34Z
TLE epoch observation values (Epoch: 2025-09-15T11:34:18.435Z)
Latitude
11.26043°
Longitude
-179.57228°
Altitude
1,435.148 km
Speed
7.151 km/s
True Right ascension
23h 14m 45s
True Declination
11° 12' 02"
Sunlit
Object was in full shadow 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
13:54:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,482.162 km
Perigee altitude
1,407.459 km
Semi-major axis
7,822.947 km
Eccentricity
0.00477
Inclination
102.0142°
RAAN
351.1072°
Arg. of periapsis
303.1806°
True anomaly
68.37756°
Mean anomaly
67.8696°
Eccentric anomaly
68.12346°
Mean motion
3.13681 °/min
Orbital period
114.77 mins
BSTAR
0.000018149
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Other satellites on launch #114 in the year 1967 (1967-11-10 UTC)

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