OV1-19, 3825
Orbit data source: Space-Track
OV1-19, 3825 is a payload satellite owned by USAF OAR (US) that was launched on Tue, 18 Mar 1969 UTC via an ATLAS F 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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3825 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
GD/Convair
Mission
Spacecraft
Bus & Motor
OV1, Unknown motor
Mass
123 kg wet, 123 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: 6 hours ago
TLE from 6 hours ago
0 OV1-19
1 03825U 69025C 26095.31591452 .00000798 00000-0 40161-3 0 9991
2 03825 104.7379 231.1034 2675522 118.7168 270.8316 9.58441360978265Epoch: 2026-04-05T07:34Z
TLE epoch observation values (Epoch: 2026-04-05T07:34:55.014Z)
Latitude
-0.00003°
Longitude
-76.24891°
Altitude
3,593.766 km
Speed
6.115 km/s
True Right ascension
15h 24m 24s
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
19:19:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
5,485.722 km
Perigee altitude
477.326 km
Semi-major axis
9,359.661 km
Eccentricity
0.26755
Inclination
104.7379°
RAAN
231.1034°
Arg. of periapsis
118.7168°
True anomaly
241.37613°
Mean anomaly
270.8316°
Eccentric anomaly
255.95994°
Mean motion
2.39692 °/min
Orbital period
150.19 mins
BSTAR
0.00040161
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Other satellites on launch #25 in the year 1969 (1969-03-18 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.OV1-19 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 | 2026-04-05 23:15:49.486Z | 332.716° NNW | 2026-04-05 23:17:49.486Z | 286.571° WNW | 18.586° | 2026-04-05 23:19:49.486Z | 252.843° W |
| 9 mins | 2026-04-06 06:21:49.486Z | 91.054° ESE | 2026-04-06 06:26:49.486Z | 60.484° ENE | 16.744° | 2026-04-06 06:30:49.486Z | 23.637° NE |
| 21 mins | 2026-04-06 08:39:49.486Z | 161.072° S | 2026-04-06 08:53:49.486Z | 229.051° WSW | 44.238° | 2026-04-06 09:00:49.486Z | 334.263° NNW |
| 7 mins | 2026-04-06 11:15:49.486Z | 238.115° WSW | 2026-04-06 11:18:49.486Z | 250.98° W | 11.892° | 2026-04-06 11:22:49.486Z | 272.129° WNW |
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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