SDA_1682, 65992
Orbit data source: Space-Track
SDA_1682, 65992 is a payload satellite owned by SDA (US) in LEO that was launched on Wed, 15 Oct 2025 UTC via an FALCON 9 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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65992 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
LMSSD/TERRAN
Mission
Operational Defense Communications
Bus & Motor
LM-T1TL, Unknown motor
Mass
~400 kg wet, ~400 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.8 m
Radar Cross Section
0.674 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 SDA_1682
1 65992U 25230U 26171.39773230 .00000107 00000-0 94760-4 0 9992
2 65992 81.3013 209.6029 0001143 103.2128 256.9153 13.78093862 34200Epoch: 2026-06-20T09:32Z
TLE epoch observation values (Epoch: 2026-06-20T09:32:44.070Z)
Latitude
-0.00002°
Longitude
157.80634°
Altitude
973.703 km
Speed
7.365 km/s
True Right ascension
13h 58m 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
07:12:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
968.709 km
Perigee altitude
967.03 km
Semi-major axis
7,346.007 km
Eccentricity
0.00011
Inclination
81.3013°
RAAN
209.6029°
Arg. of periapsis
103.2128°
True anomaly
256.90254°
Mean anomaly
256.9153°
Eccentric anomaly
256.90892°
Mean motion
3.4472 °/min
Orbital period
104.43 mins
BSTAR
0.00009476
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Other satellites on launch #230 in the year 2025 (2025-10-15 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.SDA_1682 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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-06-21 03:04:16.964Z | 174.457° S | 2026-06-21 03:10:16.964Z | 70.955° E | 41.672° | 2026-06-21 03:15:16.964Z | 16.391° NNE |
| 6 mins | 2026-06-21 04:53:16.964Z | 264.102° W | 2026-06-21 04:56:16.964Z | 298.769° NW | 17.682° | 2026-06-21 04:59:16.964Z | 330.553° NNW |
| 10 mins | 2026-06-21 14:01:16.964Z | 1.205° NNE | 2026-06-21 14:06:16.964Z | 101.973° ESE | 41.163° | 2026-06-21 14:11:16.964Z | 158.231° S |
| 6 mins | 2026-06-21 15:48:16.964Z | 302.349° NW | 2026-06-21 15:50:16.964Z | 280.04° WNW | 17.254° | 2026-06-21 15:54:16.964Z | 237.632° WSW |
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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