DB-PRECISIONFLIGHTWORKSP, 68466
Orbit data source: Space-Track
DB-PRECISIONFLIGHTWORKSP, 68466 is a payload satellite owned by NearSpaceLaunch (US) in SSO that was launched on Mon, 30 Mar 2026 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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68466 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
NearSpaceLaunch
Mission
Operational spacecraft
Bus & Motor
THINSAT 0.5U, Unknown motor
Mass
0.5 kg wet, 0.5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 DB-PRECISIONFLIGHTWORKSP
1 68466U 26067BC 26171.42112218 .00006207 00000-0 31154-3 0 9991
2 68466 97.4489 129.6599 0008103 75.6996 284.5137 15.17634976 12279Epoch: 2026-06-20T10:06Z
TLE epoch observation values (Epoch: 2026-06-20T10:06:24.956Z)
Latitude
-0.00001°
Longitude
69.41993°
Altitude
514.681 km
Speed
7.607 km/s
True Right ascension
08h 38m 38s
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
12:42:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
515.543 km
Perigee altitude
504.38 km
Semi-major axis
6,888.098 km
Eccentricity
0.00081
Inclination
97.4489°
RAAN
129.6599°
Arg. of periapsis
75.6996°
True anomaly
284.42379°
Mean anomaly
284.5137°
Eccentric anomaly
284.46875°
Mean motion
3.79659 °/min
Orbital period
94.82 mins
BSTAR
0.00031154
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Other satellites on launch #67 in the year 2026 (2026-03-30 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.DB-PRECISIONFLIGHTWORKSP 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-22 10:08:32.541Z | 10.568° NNE | 2026-06-22 10:11:32.541Z | 247.825° W | 44.854° | 2026-06-22 10:14:32.541Z | 195° SSW |
| 5 mins | 2026-06-22 20:48:32.541Z | 123.862° SE | 2026-06-22 20:50:32.541Z | 63.575° ENE | 30.206° | 2026-06-22 20:53:32.541Z | 6.726° NNE |
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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