TITAN 3C TRANSTAGE R/B, 2770
Orbit data source: Space-Track
TITAN 3C TRANSTAGE R/B, 2770 is space debris in HEO originally from a launch on Fri, 28 Apr 1967 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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2770 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: in 14 hours
TLE from in 14 hours
0 TITAN 3C TRANSTAGE R/B
1 02770U 67040F 26084.86294032 -.00000968 00000-0 00000-0 0 9991
2 02770 16.4300 210.0562 7907201 350.6955 359.5255 0.50944711 22871Epoch: 2026-03-25T20:42Z
TLE epoch observation values (Epoch: 2026-03-25T20:42:38.043Z)
Latitude
-2.35991°
Longitude
67.99582°
Altitude
7,317.22 km
Speed
7.224 km/s
True Right ascension
13h 27m 53s
True Declination
-2° 21' 09"
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
11:23:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
112,211.61 km
Perigee altitude
7,481.344 km
Semi-major axis
66,224.614 km
Eccentricity
0.79072
Inclination
16.43°
RAAN
210.0562°
Arg. of periapsis
350.6955°
True anomaly
353.38081°
Mean anomaly
359.5255°
Eccentric anomaly
357.73493°
Mean motion
0.12735 °/min
Orbital period
2,826.76 mins
BSTAR
0
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Other satellites on launch #40 in the year 1967 (1967-04-28 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.TITAN 3C TRANSTAGE 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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| TITAN 3C TRANSTAGE R/B is likely not visible in the next few days. |
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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