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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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Identifier
68458, 2026-067AU
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
Cal Poly
Mission
Operational spacecraft
Bus & Motor
CUBESAT 3U, Unknown motor
Mass
~5 kg wet, ~5 kg dry
Launch date (UTC)
2026-03-30 (1 month ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
RCS unknown

Expand to show TLE details & history
Last TLE update: 21 hours ago

TLE from 21 hours ago
0 SAL-E
1 68458U 26067AU  26126.83803605  .00006949  00000-0  35303-3 0  9997
2 68458  97.4458  85.8270 0005014 198.2049 161.9006 15.17180860  5660
Epoch: 2026-05-06T20:06Z
TLE epoch observation values (Epoch: 2026-05-06T20:06:46.314Z)
Latitude
-0.00001°
Longitude
-80.55876°
Altitude
520.737 km
Speed
7.601 km/s
True Right ascension
05h 43m 18s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
01:02:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
514.791 km
Perigee altitude
507.883 km
Semi-major axis
6,889.474 km
Eccentricity
0.0005
Inclination
97.4458°
RAAN
85.827°
Arg. of periapsis
198.2049°
True anomaly
161.91844°
Mean anomaly
161.9006°
Eccentric anomaly
161.90952°
Mean motion
3.79546 °/min
Orbital period
94.85 mins
BSTAR
0.00035303
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