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: 17 hours ago
TLE from 17 hours ago
0 TIMATION 1
1 02847U 67053E 25295.57634293 .00000362 00000-0 26831-3 0 9998
2 02847 69.9674 1.9152 0006698 346.5637 13.5293 14.02854618980464Epoch: 2025-10-22T13:49Z
TLE epoch observation values (Epoch: 2025-10-22T13:49:56.029Z)
Latitude
0.00003°
Longitude
123.18379°
Altitude
881.515 km
Speed
7.414 km/s
True Right ascension
00h 07m 39s
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
01:46:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
886.83 km
Perigee altitude
877.104 km
Semi-major axis
7,260.104 km
Eccentricity
0.00067
Inclination
69.9674°
RAAN
1.9152°
Arg. of periapsis
346.5637°
True anomaly
13.54727°
Mean anomaly
13.5293°
Eccentric anomaly
13.53828°
Mean motion
3.50856 °/min
Orbital period
102.61 mins
BSTAR
0.00026831
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-10-23 07:05:49.800Z | 246.324° WSW | 2025-10-23 07:10:49.800Z | 307.668° NW | 26.057° | 2025-10-23 07:14:49.800Z | 359.308° N |
| 8 mins | 2025-10-23 14:20:49.800Z | 7.641° NNE | 2025-10-23 14:23:49.800Z | 45.375° ENE | 23.118° | 2025-10-23 14:28:49.800Z | 106.518° ESE |
| 9 mins | 2025-10-23 16:05:49.800Z | 318.675° NNW | 2025-10-23 16:09:49.800Z | 246.193° WSW | 37.787° | 2025-10-23 16:14:49.800Z | 178.78° S |
| 9 mins | 2025-10-24 05:18:49.800Z | 178.777° S | 2025-10-24 05:22:49.800Z | 118.268° SE | 38.015° | 2025-10-24 05:27:49.800Z | 37.052° NE |
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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