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: 7 hours ago
TLE from 7 hours ago
0 TIMATION 1
1 2847U 67053E 25312.47478079 .00000223 00000-0 17907-3 0 9995
2 2847 69.9651 325.3134 0007895 327.2338 32.8280 14.02865121982830Epoch: 2025-11-08T11:23Z
TLE epoch observation values (Epoch: 2025-11-08T11:23:41.060Z)
Latitude
-0.00005°
Longitude
106.48843°
Altitude
881.391 km
Speed
7.414 km/s
True Right ascension
21h 41m 15s
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
14:59:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
887.663 km
Perigee altitude
876.199 km
Semi-major axis
7,260.068 km
Eccentricity
0.00079
Inclination
69.9651°
RAAN
325.3134°
Arg. of periapsis
327.2338°
True anomaly
32.87709°
Mean anomaly
32.828°
Eccentric anomaly
32.85254°
Mean motion
3.50859 °/min
Orbital period
102.61 mins
BSTAR
0.00017907
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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 | 2025-11-09 01:12:10.856Z | 145.458° SSE | 2025-11-09 01:16:10.856Z | 99.385° ESE | 19.615° | 2025-11-09 01:20:10.856Z | 55.397° ENE |
| 10 mins | 2025-11-09 02:56:10.856Z | 224.255° SW | 2025-11-09 03:00:10.856Z | 279.107° WNW | 38.878° | 2025-11-09 03:06:10.856Z | 15.863° NNE |
| 4 mins | 2025-11-09 10:12:10.856Z | 25.89° NE | 2025-11-09 10:14:10.856Z | 48.025° ENE | 13.871° | 2025-11-09 10:16:10.856Z | 69.551° E |
| 10 mins | 2025-11-09 11:55:10.856Z | 338.114° N | 2025-11-09 12:00:10.856Z | 94.182° ESE | 44.565° | 2025-11-09 12:05:10.856Z | 152.728° SSE |
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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