ATLAS AGENA R/B, 27785
Orbit data source: Space-Track
ATLAS AGENA R/B, 27785 is space debris in GEO originally from a launch on Tue, 06 Aug 1968 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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27785 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 ATLAS AGENA R/B
1 27785U 68063B 25303.24395011 -.00000186 00000-0 00000-0 0 9996
2 27785 4.9716 269.5424 1022647 258.4546 89.7920 1.01773727 24046Epoch: 2025-10-30T05:51Z
TLE epoch observation values (Epoch: 2025-10-30T05:51:17.289Z)
Latitude
0°
Longitude
142.76909°
Altitude
35,767.762 km
Speed
3.061 km/s
True Right ascension
17h 57m 35s
True Declination
0° 00' 00"
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
18:19:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
39,641.365 km
Perigee altitude
31,102.271 km
Semi-major axis
41,749.955 km
Eccentricity
0.10226
Inclination
4.9716°
RAAN
269.5424°
Arg. of periapsis
258.4546°
True anomaly
101.43539°
Mean anomaly
89.792°
Eccentric anomaly
95.62314°
Mean motion
0.25442 °/min
Orbital period
1,414.96 mins
BSTAR
0
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Other satellites on launch #63 in the year 1968 (1968-08-06 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.ATLAS AGENA R/B Visibility
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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. |
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| ATLAS AGENA R/B is likely not visible in the next few days. |
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27785 neighbors
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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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
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