LCS 1, 1361
Orbit data source: Space-Track
LCS 1, 1361 is an American payload satellite in LEO that was launched on Thu, 06 May 1965 UTC via a TITAN IIIA launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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1361 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
ROHR/MITLL
Mission
Operational spacecraft
Bus & Motor
LCS, Unknown motor
Mass
34 kg wet, 34 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
SPHERE, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 15 hours ago
TLE from 15 hours ago
0 LCS 1
1 01361U 65034C 26283.58931148 .00000006 00000-0 -35622-3 0 9997
2 01361 32.1406 263.0250 0010918 173.1517 186.9130 9.89311010221310Epoch: 2026-10-10T14:08Z
TLE epoch observation values (Epoch: 2026-10-10T14:08:36.511Z)
Latitude
-0.00005°
Longitude
31.67853°
Altitude
2,796.759 km
Speed
6.59 km/s
True Right ascension
17h 32m 05s
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
23:31:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,800.647 km
Perigee altitude
2,780.626 km
Semi-major axis
9,168.773 km
Eccentricity
0.00109
Inclination
32.1406°
RAAN
263.025°
Arg. of periapsis
173.1517°
True anomaly
186.89796°
Mean anomaly
186.913°
Eccentric anomaly
186.90548°
Mean motion
2.47216 °/min
Orbital period
145.62 mins
BSTAR
-0.00035622
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Other satellites on launch #34 in the year 1965 (1965-05-06 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.LCS 1 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. |
|---|---|---|---|---|---|---|---|
| 21 mins | 2026-10-11 05:12:18.715Z | 241.913° WSW | 2026-10-11 05:18:18.715Z | 181.127° SSW | 65.651° | 2026-10-11 05:33:18.715Z | 104.72° ESE |
| 28 mins | 2026-10-11 07:42:18.715Z | 269.761° W | 2026-10-11 07:55:18.715Z | 207.133° SW | 48.714° | 2026-10-11 08:10:18.715Z | 134.991° SE |
| 18 mins | 2026-10-11 10:23:18.715Z | 256.437° W | 2026-10-11 10:32:18.715Z | 218.658° SW | 20.14° | 2026-10-11 10:41:18.715Z | 181.755° SSW |
| 23 mins | 2026-10-12 00:09:18.715Z | 193.687° SSW | 2026-10-12 00:20:18.715Z | 144.815° SSE | 29.352° | 2026-10-12 00:32:18.715Z | 93.004° ESE |
| 29 mins | 2026-10-12 02:43:18.715Z | 234.592° WSW | 2026-10-12 02:57:18.715Z | 159.988° S | 56.969° | 2026-10-12 03:12:18.715Z | 90.267° ESE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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