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: 10 hours ago
TLE from 10 hours ago
0 SAL-E
1 68458U 26067AU 26264.86153359 .00005061 00000-0 24523-3 0 9993
2 68458 97.4580 221.7526 0007820 95.2045 265.0082 15.18958224 26605Epoch: 2026-09-21T20:40Z
TLE epoch observation values (Epoch: 2026-09-21T20:40:36.502Z)
Latitude
-0.00001°
Longitude
-89.13478°
Altitude
512.548 km
Speed
7.607 km/s
True Right ascension
14h 47m 00s
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
23:52:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
511.341 km
Perigee altitude
500.574 km
Semi-major axis
6,884.094 km
Eccentricity
0.00078
Inclination
97.458°
RAAN
221.7526°
Arg. of periapsis
95.2045°
True anomaly
264.91894°
Mean anomaly
265.0082°
Eccentric anomaly
264.96357°
Mean motion
3.79991 °/min
Orbital period
94.74 mins
BSTAR
0.00024523
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-09-22 09:53:20.657Z | 21.875° NNE | 2026-09-22 09:56:20.657Z | 96.149° ESE | 59.133° | 2026-09-22 09:59:20.657Z | 178.592° S |
| 4 mins | 2026-09-22 20:33:20.657Z | 102.762° ESE | 2026-09-22 20:34:20.657Z | 80.329° E | 23.156° | 2026-09-22 20:37:20.657Z | 19.968° NNE |
| 4 mins | 2026-09-22 22:07:20.657Z | 237.99° WSW | 2026-09-22 22:08:20.657Z | 259.445° W | 20.353° | 2026-09-22 22:11:20.657Z | 314.311° NW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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