OPS 5712 (P/L 160), 2826
Orbit data source: Space-Track
OPS 5712 (P/L 160), 2826 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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2826 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
NRL
Mission
Operational spacecraft
Bus & Motor
NRL 14"?, Unknown motor
Mass
5 kg wet, 5 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: 13 hours ago
TLE from 13 hours ago
0 OPS 5712 (P/L 160)
1 02826U 67053A 25286.96515264 .00011679 00000-0 18392-2 0 9999
2 02826 69.9183 279.6757 0004757 321.3387 38.7417 14.72636603 29918Epoch: 2025-10-13T23:09Z
TLE epoch observation values (Epoch: 2025-10-13T23:09:49.188Z)
Latitude
-0°
Longitude
-90.53962°
Altitude
652.445 km
Speed
7.533 km/s
True Right ascension
18h 38m 42s
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
07:05:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
653.988 km
Perigee altitude
647.3 km
Semi-major axis
7,028.781 km
Eccentricity
0.00048
Inclination
69.9183°
RAAN
279.6757°
Arg. of periapsis
321.3387°
True anomaly
38.77583°
Mean anomaly
38.7417°
Eccentric anomaly
38.75876°
Mean motion
3.68318 °/min
Orbital period
97.74 mins
BSTAR
0.0018392
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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.OPS 5712 (P/L 160) 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-14 23:45:40.766Z | 125.881° SE | 2025-10-14 23:47:40.766Z | 97.539° ESE | 14.169° | 2025-10-14 23:49:40.766Z | 70.91° E |
| 7 mins | 2025-10-15 01:23:40.766Z | 224.892° SW | 2025-10-15 01:26:40.766Z | 282.819° WNW | 38.457° | 2025-10-15 01:30:40.766Z | 12.527° NNE |
| 6 mins | 2025-10-15 09:57:40.766Z | 4.585° NNE | 2025-10-15 09:59:40.766Z | 45.596° ENE | 31.654° | 2025-10-15 10:03:40.766Z | 124.981° SE |
| 5 mins | 2025-10-15 11:37:40.766Z | 291.279° WNW | 2025-10-15 11:39:40.766Z | 259.763° W | 19.314° | 2025-10-15 11:42:40.766Z | 214.221° SW |
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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