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: 12 hours ago
TLE from 12 hours ago
0 TIMATION 1
1 2847U 67053E 25295.21983431 .00000351 00000-0 26158-3 0 9990
2 2847 69.9674 2.6873 0006675 347.0105 13.0831 14.02854368980413Epoch: 2025-10-22T05:16Z
TLE epoch observation values (Epoch: 2025-10-22T05:16:33.684Z)
Latitude
-0.00002°
Longitude
-107.34963°
Altitude
881.523 km
Speed
7.414 km/s
True Right ascension
00h 10m 44s
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
12:34:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
886.814 km
Perigee altitude
877.122 km
Semi-major axis
7,260.105 km
Eccentricity
0.00067
Inclination
69.9674°
RAAN
2.6873°
Arg. of periapsis
347.0105°
True anomaly
13.10043°
Mean anomaly
13.0831°
Eccentric anomaly
13.09176°
Mean motion
3.50856 °/min
Orbital period
102.61 mins
BSTAR
0.00026158
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-10-23 05:20:39.755Z | 173.942° S | 2025-10-23 05:25:39.755Z | 101.954° ESE | 34.007° | 2025-10-23 05:30:39.755Z | 39.064° NE |
| 8 mins | 2025-10-23 07:07:39.755Z | 260.22° W | 2025-10-23 07:10:39.755Z | 304.579° NW | 26.078° | 2025-10-23 07:15:39.755Z | 4.586° NNE |
| 8 mins | 2025-10-23 14:20:39.755Z | 6.221° NNE | 2025-10-23 14:24:39.755Z | 58.917° ENE | 23.215° | 2025-10-23 14:28:39.755Z | 105.393° ESE |
| 9 mins | 2025-10-23 16:05:39.755Z | 319.511° NNW | 2025-10-23 16:09:39.755Z | 252.175° W | 37.836° | 2025-10-23 16:14:39.755Z | 179.322° S |
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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