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
Spacecraft
Bus & Motor
TRANSIT 5, Unknown motor
Mass
~50 kg wet, ~50 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 OPS 7218 (TRANSIT 16)
1 02807U 67048A 25303.19202308 .00000146 00000-0 21144-3 0 9996
2 02807 89.6782 355.4516 0018611 238.5919 180.6452 13.50708814876882Epoch: 2025-10-30T04:36Z
TLE epoch observation values (Epoch: 2025-10-30T04:36:30.794Z)
Latitude
59.32363°
Longitude
-111.89133°
Altitude
1,093.655 km
Speed
7.304 km/s
True Right ascension
23h 43m 57s
True Declination
59° 10' 45"
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
09:03:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,080.556 km
Perigee altitude
1,052.845 km
Semi-major axis
7,444.838 km
Eccentricity
0.00186
Inclination
89.6782°
RAAN
355.4516°
Arg. of periapsis
238.5919°
True anomaly
180.6428°
Mean anomaly
180.6452°
Eccentric anomaly
180.644°
Mean motion
3.37878 °/min
Orbital period
106.55 mins
BSTAR
0.00021144
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2025-10-30 15:34:23.509Z | 9.664° NNE | 2025-10-30 15:40:23.509Z | 80.298° E | 40.979° | 2025-10-30 15:46:23.509Z | 167.24° S |
| 7 mins | 2025-10-30 17:23:23.509Z | 320.318° NNW | 2025-10-30 17:26:23.509Z | 287.347° WNW | 20.128° | 2025-10-30 17:30:23.509Z | 245.604° WSW |
| 11 mins | 2025-10-31 03:32:23.509Z | 156.56° SSE | 2025-10-31 03:37:23.509Z | 93.149° ESE | 40.042° | 2025-10-31 03:43:23.509Z | 8.203° NNE |
| 8 mins | 2025-10-31 05:21:23.509Z | 245.035° WSW | 2025-10-31 05:24:23.509Z | 278.779° WNW | 21.02° | 2025-10-31 05:29:23.509Z | 328.961° NNW |
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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