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: 16 hours ago
TLE from 16 hours ago
0 TIMATION 1
1 2847U 67053E 25296.43196308 .00000341 00000-0 25519-3 0 9993
2 2847 69.9673 0.0621 0006745 345.5168 14.5747 14.02855165980581Epoch: 2025-10-23T10:22Z
TLE epoch observation values (Epoch: 2025-10-23T10:22:01.610Z)
Latitude
0.00003°
Longitude
172.4641°
Altitude
881.501 km
Speed
7.414 km/s
True Right ascension
00h 00m 14s
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
21:36:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
886.862 km
Perigee altitude
877.068 km
Semi-major axis
7,260.102 km
Eccentricity
0.00067
Inclination
69.9673°
RAAN
0.0621°
Arg. of periapsis
345.5168°
True anomaly
14.59417°
Mean anomaly
14.5747°
Eccentric anomaly
14.58443°
Mean motion
3.50856 °/min
Orbital period
102.61 mins
BSTAR
0.00025519
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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 | 2025-10-24 05:18:17.834Z | 180.832° SSW | 2025-10-24 05:23:17.834Z | 101.011° ESE | 38.071° | 2025-10-24 05:28:17.834Z | 35.571° NE |
| 7 mins | 2025-10-24 07:05:17.834Z | 264.594° W | 2025-10-24 07:08:17.834Z | 304.165° NW | 22.854° | 2025-10-24 07:12:17.834Z | 355.072° N |
| 8 mins | 2025-10-24 14:18:17.834Z | 3.064° NNE | 2025-10-24 14:22:17.834Z | 58.916° ENE | 26.511° | 2025-10-24 14:26:17.834Z | 110.098° ESE |
| 9 mins | 2025-10-24 16:03:17.834Z | 314.887° NW | 2025-10-24 16:07:17.834Z | 253.001° W | 33.74° | 2025-10-24 16:12:17.834Z | 186.02° SSW |
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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