OPS 7218 (TRANSIT 16), 2807
Orbit data source: Space-Track
OPS 7218 (TRANSIT 16), 2807 is a payload satellite owned by USN NAVAIR (US) in LEO that was launched on Thu, 18 May 1967 UTC via an SCOUT A 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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2807 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
APL
Mission
Defense Navigation
Bus & Motor
TRANSIT 5, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Oct Cyl + 4 Pan + 1 Rod, Unknown HBR
Radar Cross Section
7.565 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 OPS 7218 (TRANSIT 16)
1 02807U 67048A 25258.51224265 .00000092 00000-0 12766-3 0 9997
2 02807 89.6820 356.8960 0020367 17.0742 354.8168 13.50694956870859Epoch: 2025-09-15T12:17Z
TLE epoch observation values (Epoch: 2025-09-15T12:17:37.764Z)
Latitude
11.82512°
Longitude
177.83905°
Altitude
1,056.792 km
Speed
7.332 km/s
True Right ascension
23h 47m 50s
True Declination
11° 45' 33"
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
21:29:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,081.915 km
Perigee altitude
1,051.589 km
Semi-major axis
7,444.889 km
Eccentricity
0.00204
Inclination
89.682°
RAAN
356.896°
Arg. of periapsis
17.0742°
True anomaly
354.79566°
Mean anomaly
354.8168°
Eccentric anomaly
354.80624°
Mean motion
3.37875 °/min
Orbital period
106.55 mins
BSTAR
0.00012766
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Other satellites on launch #48 in the year 1967 (1967-05-18 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.OPS 7218 (TRANSIT 16) 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-09-16 06:07:25.332Z | 140.274° SSE | 2025-09-16 06:13:25.332Z | 71.285° E | 29.652° | 2025-09-16 06:18:25.332Z | 17.804° NNE |
| 9 mins | 2025-09-16 07:55:25.332Z | 221.207° SW | 2025-09-16 07:59:25.332Z | 275.951° WNW | 30.467° | 2025-09-16 08:04:25.332Z | 336.622° NNW |
| 6 mins | 2025-09-16 17:19:25.332Z | 52.802° ENE | 2025-09-16 17:21:25.332Z | 72.2° E | 14.617° | 2025-09-16 17:25:25.332Z | 109.587° ESE |
| 12 mins | 2025-09-16 19:03:25.332Z | 359.383° N | 2025-09-16 19:09:25.332Z | 224.673° SW | 44.337° | 2025-09-16 19:15:25.332Z | 187.676° SSW |
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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