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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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: 14 hours ago
TLE from 14 hours ago
0 TIMATION 1
1 2847U 67053E 26188.60303433 .00000194 00000-0 15951-3 0 9997
2 2847 69.9639 162.9663 0005384 14.1862 345.9397 14.02990327 16655Epoch: 2026-07-07T14:28Z
TLE epoch observation values (Epoch: 2026-07-07T14:28:22.166Z)
Latitude
-0.00003°
Longitude
20.30264°
Altitude
881.983 km
Speed
7.413 km/s
True Right ascension
10h 51m 51s
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
16:47:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
885.407 km
Perigee altitude
877.59 km
Semi-major axis
7,259.636 km
Eccentricity
0.00054
Inclination
69.9639°
RAAN
162.9663°
Arg. of periapsis
14.1862°
True anomaly
345.9247°
Mean anomaly
345.9397°
Eccentric anomaly
345.9322°
Mean motion
3.5089 °/min
Orbital period
102.6 mins
BSTAR
0.00015951
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-07-08 08:07:49.753Z | 3.824° NNE | 2026-07-08 08:11:49.753Z | 52.58° ENE | 22.408° | 2026-07-08 08:15:49.753Z | 101.286° ESE |
| 10 mins | 2026-07-08 09:52:49.753Z | 322.507° NNW | 2026-07-08 09:56:49.753Z | 266.91° W | 38.5° | 2026-07-08 10:02:49.753Z | 175.626° S |
| 9 mins | 2026-07-08 23:06:49.753Z | 173.936° S | 2026-07-08 23:10:49.753Z | 100.07° ESE | 36.845° | 2026-07-08 23:15:49.753Z | 36.497° NE |
| 7 mins | 2026-07-09 00:52:49.753Z | 263.845° W | 2026-07-09 00:55:49.753Z | 305.105° NW | 23.767° | 2026-07-09 00:59:49.753Z | 356.348° N |
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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