SAL-E, 68458
Orbit data source: Space-Track
SAL-E, 68458 is a payload satellite owned by Cal Poly (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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68458 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Cal Poly
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
~5 kg wet, ~5 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 SAL-E
1 68458U 26067AU 26255.30908575 .00005439 00000-0 26419-3 0 9995
2 68458 97.4570 212.3249 0007395 120.2650 239.9317 15.18845387 25155Epoch: 2026-09-12T07:25Z
TLE epoch observation values (Epoch: 2026-09-12T07:25:05.008Z)
Latitude
-0.00006°
Longitude
109.7341°
Altitude
514.972 km
Speed
7.605 km/s
True Right ascension
14h 09m 17s
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
09:09:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.39 km
Perigee altitude
501.207 km
Semi-major axis
6,884.435 km
Eccentricity
0.00074
Inclination
97.457°
RAAN
212.3249°
Arg. of periapsis
120.265°
True anomaly
239.8584°
Mean anomaly
239.9317°
Eccentric anomaly
239.89505°
Mean motion
3.79962 °/min
Orbital period
94.75 mins
BSTAR
0.00026419
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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.SAL-E 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-09-12 21:47:18.162Z | 209.495° SW | 2026-09-12 21:49:18.162Z | 265.662° W | 35.161° | 2026-09-12 21:52:18.162Z | 327.354° NNW |
| 4 mins | 2026-09-13 10:52:18.162Z | 327.947° NNW | 2026-09-13 10:54:18.162Z | 281.81° WNW | 23.472° | 2026-09-13 10:56:18.162Z | 242.905° 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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Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in descending order |
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