DB-WALI-WMU, 68443
Orbit data source: Space-Track
DB-WALI-WMU, 68443 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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68443 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
NearSpaceLaunch
Mission
Operational Commercial Technology
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
Box + 2 Pan, 1.1 m
Radar Cross Section
0.017 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 DB-WALI-WMU
1 68443U 26067AD 26247.35186014 .00002761 00000-0 13822-3 0 9990
2 68443 97.4629 204.5892 0005542 138.0555 222.1104 15.18222920 23949Epoch: 2026-09-04T08:26Z
TLE epoch observation values (Epoch: 2026-09-04T08:26:40.716Z)
Latitude
-0.00003°
Longitude
94.44263°
Altitude
517.132 km
Speed
7.603 km/s
True Right ascension
13h 38m 21s
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
06:06:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.998 km
Perigee altitude
504.366 km
Semi-major axis
6,886.319 km
Eccentricity
0.00055
Inclination
97.4629°
RAAN
204.5892°
Arg. of periapsis
138.0555°
True anomaly
222.06784°
Mean anomaly
222.1104°
Eccentric anomaly
222.08912°
Mean motion
3.79807 °/min
Orbital period
94.79 mins
BSTAR
0.00013822
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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-WALI-WMU 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 | 2026-09-05 20:57:20.573Z | 146.837° SSE | 2026-09-05 21:00:20.573Z | 78.027° E | 36.851° | 2026-09-05 21:03:20.573Z | 2.55° NNE |
| 5 mins | 2026-09-06 10:03:20.573Z | 16.827° NNE | 2026-09-06 10:05:20.573Z | 47.547° ENE | 43.452° | 2026-09-06 10:08:20.573Z | 187.728° SSW |
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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