SHARJAHSAT-2, 68444
Orbit data source: Space-Track
SHARJAHSAT-2, 68444 is a payload satellite owned by Sharjah SAAST (AE) 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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68444 intel report (Beta)
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Identifier
Orbit
Country
AE / UAERelated business
Manufacturer
Sharjah SAAST
Mission
Operational Amateur Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
~10 kg wet, ~10 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.035 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 SHARJAHSAT-2
1 68444U 26067AE 26221.86621466 .00003451 00000-0 16581-3 0 9996
2 68444 97.4605 179.7453 0003024 119.8507 240.3028 15.19499015 20099Epoch: 2026-08-09T20:47Z
TLE epoch observation values (Epoch: 2026-08-09T20:47:20.946Z)
Latitude
-0.00009°
Longitude
-90.44903°
Altitude
511.474 km
Speed
7.608 km/s
True Right ascension
11h 58m 58s
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
16:19:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
506.404 km
Perigee altitude
502.241 km
Semi-major axis
6,882.459 km
Eccentricity
0.0003
Inclination
97.4605°
RAAN
179.7453°
Arg. of periapsis
119.8507°
True anomaly
240.2727°
Mean anomaly
240.3028°
Eccentric anomaly
240.28775°
Mean motion
3.80126 °/min
Orbital period
94.71 mins
BSTAR
0.00016581
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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.SHARJAHSAT-2 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 | 2026-08-10 10:00:03.032Z | 19.16° NNE | 2026-08-10 10:03:03.032Z | 131.454° SE | 42.514° | 2026-08-10 10:06:03.032Z | 184.596° SSW |
| 4 mins | 2026-08-10 20:39:03.032Z | 114.743° SE | 2026-08-10 20:41:03.032Z | 66.971° ENE | 24.076° | 2026-08-10 20:43:03.032Z | 23.309° NE |
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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