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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3036 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
UTC
Mission
Spacecraft
Bus & Motor
FW4, Unknown motor
Mass
~40 kg wet, ~40 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
CYL, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 DELTA 1 R/B
1 03036U 67114B 26305.57276022 -.00000035 00000-0 73747-4 0 9999
2 03036 102.0193 48.4848 0047958 236.4154 134.5371 12.54141288699570Epoch: 2026-11-01T13:44Z
TLE epoch observation values (Epoch: 2026-11-01T13:44:46.483Z)
Latitude
11.04844°
Longitude
159.05801°
Altitude
1,475.457 km
Speed
7.114 km/s
True Right ascension
03h 04m 27s
True Declination
10° 59' 23"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
10:34:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,482.295 km
Perigee altitude
1,407.261 km
Semi-major axis
7,822.915 km
Eccentricity
0.0048
Inclination
102.0193°
RAAN
48.4848°
Arg. of periapsis
236.4154°
True anomaly
134.92718°
Mean anomaly
134.5371°
Eccentric anomaly
134.7323°
Mean motion
3.13682 °/min
Orbital period
114.77 mins
BSTAR
0.000073747
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Other satellites on launch #114 in the year 1967 (1967-11-10 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.DELTA 1 R/B 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. |
|---|---|---|---|---|---|---|---|
| 14 mins | 2026-11-02 19:02:53.030Z | 35.225° NE | 2026-11-02 19:09:53.030Z | 100.773° ESE | 39.02° | 2026-11-02 19:16:53.030Z | 164.237° S |
| 14 mins | 2026-11-02 20:55:53.030Z | 3.795° NNE | 2026-11-02 21:02:53.030Z | 289.731° WNW | 47.241° | 2026-11-02 21:09:53.030Z | 228.222° WSW |
| 14 mins | 2026-11-03 06:00:53.030Z | 133.825° SE | 2026-11-03 06:07:53.030Z | 56.039° ENE | 52.878° | 2026-11-03 06:14:53.030Z | 352.774° N |
| 14 mins | 2026-11-03 07:53:53.030Z | 202.561° SW | 2026-11-03 07:59:53.030Z | 255.106° W | 35.151° | 2026-11-03 08:07:53.030Z | 325.22° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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