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

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 DELTA 1 R/B
1 03036U 67114B   25311.14421020 -.00000019  00000-0  17275-3 0  9993
2 03036 102.0143  44.4497 0048095 202.3320 231.2504 12.54134973654512
Epoch: 2025-11-07T03:27Z
TLE epoch observation values (Epoch: 2025-11-07T03:27:39.761Z)
Latitude
69.48681°
Longitude
-88.53158°
Altitude
1,482.765 km
Speed
7.118 km/s
True Right ascension
00h 39m 54s
True Declination
69° 23' 03"
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
13:16:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,482.428 km
Perigee altitude
1,407.18 km
Semi-major axis
7,822.941 km
Eccentricity
0.00481
Inclination
102.0143°
RAAN
44.4497°
Arg. of periapsis
202.332°
True anomaly
230.8222°
Mean anomaly
231.2504°
Eccentric anomaly
231.03614°
Mean motion
3.13681 °/min
Orbital period
114.77 mins
BSTAR
0.00017275
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Other satellites on launch #114 in the year 1967 (1967-11-10 UTC)

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