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OPS 6026 (DMSP 4A F1), 2418

Orbit data source: Space-Track

OPS 6026 (DMSP 4A F1), 2418 is a payload satellite owned by USAF SSD (US) in SSO that was launched on Fri, 16 Sep 1966 UTC via a THOR BURNER 2 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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Identifier
2418, 1966-082A
Orbit
SSO
Last TLE update
9 hours ago
Origin
Manufacturer
RCA/East Windsor
Mission
Non-operational Defense Weather
Bus & Motor
DMSP BLOCK 4A, Unknown motor
Mass
79 kg wet, 79 kg dry
Launch date (UTC)
1966-09-16 (59 years ago)
Launch vehicle
THOR BURNER 2
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Oct Cyl, 0.8 m
Radar Cross Section
0.655 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history

TLE from 9 hours ago
0 OPS 6026 (DMSP 4A F1)
1  2418U 66082A   25128.96564618  .00000666  00000-0  19381-3 0  9993
2  2418  98.2887 286.3894 0116317 168.2310 192.1642 14.43515890 74678
Epoch: 2025-05-08T23:10Z
Definitive object data (Epoch: 2025-05-08T23:10:31.829Z)
Latitude
-0.00007°
Longitude
71.72822°
Altitude
830.94 km
Speed
7.395 km/s
True Right ascension
19h 05m 33s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at TLE epoch
Visualization TLE readout
Latitude
62.29848°
Longitude
-91.89234°
Altitude
704.261 km
Speed
7.538 km/s
Apparent Right ascension
05h 45m 28s
Apparent Declination
16° 56' 25"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
16:11:12
Azimuth
334.057° NNW
Elevation
-29.049°
Doppler factor
1
Orbital elements
Apogee altitude
826.855 km
Perigee altitude
661.17 km
Semi-major axis
7,122.149 km
Eccentricity
0.0116317
Inclination
98.2887°
RAAN
286.3894°
Arg. of periapsis
168.231°
True anomaly
191.88728°
Mean anomaly
192.1642°
Eccentric anomaly
192.02535°
Mean motion
3.61099 °/min
BSTAR
0.00019381
Orbital period
99.7 mins
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Other satellites on launch #82 in the year 1966 (1966-09-16 UTC)

OPS 6026 (DMSP 4A F1) Visibility forecast

Observer location: undefined°, undefined°

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.
7 mins2025-05-09 09:18:06.822Z113.854° SE2025-05-09 09:22:06.822Z63.572° ENE20.396°2025-05-09 09:25:06.822Z22.923° NE
8 mins2025-05-09 10:57:06.822Z196.908° SSW2025-05-09 11:00:06.822Z254.133° W35.901°2025-05-09 11:05:06.822Z333.885° NNW
7 mins2025-05-09 23:04:06.822Z29.236° NE2025-05-09 23:07:06.822Z113.714° SE39.489°2025-05-09 23:11:06.822Z178.813° S
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