DODGE 1, 2867
Orbit data source: Space-Track
DODGE 1, 2867 is a payload satellite owned by USN NAVAIR (US) in GEO that was launched on Sat, 01 Jul 1967 UTC via a TITAN IIIC launch vehicle from the Air Force Eastern Test Range (AFETR). 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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2867 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
APL
Mission
Spacecraft
Bus & Motor
DODGE, Unknown motor
Mass
195 kg wet, 195 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: 8 hours ago
TLE from 8 hours ago
0 DODGE 1
1 2867U 67066F 26121.44848751 -.00000042 00000-0 00000+0 0 9997
2 2867 2.3875 99.1664 0053292 191.9913 264.5787 1.09167207132872Epoch: 2026-05-01T10:45Z
TLE epoch observation values (Epoch: 2026-05-01T10:45:49.320Z)
Latitude
2.35489°
Longitude
174.29725°
Altitude
33,483.48 km
Speed
3.161 km/s
True Right ascension
13h 00m 32s
True Declination
2° 21' 09"
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
02:43:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,677.252 km
Perigee altitude
33,252.589 km
Semi-major axis
39,843.058 km
Eccentricity
0.00533
Inclination
2.3875°
RAAN
99.1664°
Arg. of periapsis
191.9913°
True anomaly
263.97114°
Mean anomaly
264.5787°
Eccentric anomaly
264.27488°
Mean motion
0.27291 °/min
Orbital period
1,319.13 mins
BSTAR
0
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Other satellites on launch #66 in the year 1967 (1967-07-01 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.DODGE 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. |
|---|---|---|---|---|---|---|---|
| 1189 mins | 2026-05-01 23:15:45.706Z | 250.148° W | 2026-05-02 19:04:45.706Z | 227.161° WSW | 25.247° | 2026-05-02 19:04:45.706Z | 227.161° WSW |
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2867 neighbors
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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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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