TIMATION 1, 2847
Orbit data source: Space-Track
TIMATION 1, 2847 is a payload satellite owned by NRL (US) in LEO that was launched on Wed, 31 May 1967 UTC via a THOR SLV-2 AGENA D launch vehicle from the Air Force Western Test Range (AFWTR). 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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2847 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
NRL
Mission
Spacecraft
Bus & Motor
TIMATION, Unknown motor
Mass
39 kg wet, 39 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 TIMATION 1
1 2847U 67053E 25311.76176899 .00000215 00000-0 17388-3 0 9995
2 2847 69.9651 326.8579 0007851 327.9626 32.1005 14.02864695982730Epoch: 2025-11-07T18:16Z
TLE epoch observation values (Epoch: 2025-11-07T18:16:56.840Z)
Latitude
-0.00002°
Longitude
5.41997°
Altitude
881.38 km
Speed
7.414 km/s
True Right ascension
21h 47m 25s
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
19:20:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
887.632 km
Perigee altitude
876.232 km
Semi-major axis
7,260.069 km
Eccentricity
0.00079
Inclination
69.9651°
RAAN
326.8579°
Arg. of periapsis
327.9626°
True anomaly
32.14835°
Mean anomaly
32.1005°
Eccentric anomaly
32.12442°
Mean motion
3.50859 °/min
Orbital period
102.61 mins
BSTAR
0.00017388
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Other satellites on launch #53 in the year 1967 (1967-05-31 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.TIMATION 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-08 01:15:49.011Z | 130.49° SE | 2025-11-08 01:18:49.011Z | 95.919° ESE | 16.258° | 2025-11-08 01:21:49.011Z | 63.698° ENE |
| 9 mins | 2025-11-08 02:58:49.011Z | 217.546° SW | 2025-11-08 03:02:49.011Z | 286.938° WNW | 42.478° | 2025-11-08 03:07:49.011Z | 17.515° NNE |
| 10 mins | 2025-11-08 11:57:49.011Z | 342.91° N | 2025-11-08 12:02:49.011Z | 94.177° ESE | 42.136° | 2025-11-08 12:07:49.011Z | 146.21° SSE |
| 5 mins | 2025-11-08 13:44:49.011Z | 283.363° WNW | 2025-11-08 13:46:49.011Z | 259.864° W | 16.154° | 2025-11-08 13:49:49.011Z | 226.838° WSW |
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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