STPSAT-7, 68630
Orbit data source: Space-Track
STPSAT-7, 68630 is a payload satellite owned by USAF STP (US) in LEO that was launched on Tue, 07 Apr 2026 UTC via an MINOTAUR IV 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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68630 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
Aegis Aerospace
Mission
Operational spacecraft
Bus & Motor
STPSAT7, AOCS
Mass
~100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 14.5 m
Radar Cross Section
RCS unknown
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 STPSAT-7
1 68630U 26074D 26140.42439993 .00003007 00000-0 13273-3 0 9997
2 68630 60.0218 284.6789 0022629 3.4553 356.6680 15.24351184 6540Epoch: 2026-05-20T10:11Z
TLE epoch observation values (Epoch: 2026-05-20T10:11:08.153Z)
Latitude
-0.00001°
Longitude
-106.18923°
Altitude
478.813 km
Speed
7.636 km/s
True Right ascension
18h 58m 42s
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
07:16:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.481 km
Perigee altitude
476.388 km
Semi-major axis
6,870.071 km
Eccentricity
0.00226
Inclination
60.0218°
RAAN
284.6789°
Arg. of periapsis
3.4553°
True anomaly
356.65289°
Mean anomaly
356.668°
Eccentric anomaly
356.66045°
Mean motion
3.81155 °/min
Orbital period
94.45 mins
BSTAR
0.00013273
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Other satellites on launch #74 in the year 2026 (2026-04-07 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.STPSAT-7 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-05-21 11:31:01.536Z | 212.265° SW | 2026-05-21 11:35:01.536Z | 68.648° E | 41.873° | 2026-05-21 11:38:01.536Z | 42.293° NE |
| 6 mins | 2026-05-21 19:47:01.536Z | 317.528° NNW | 2026-05-21 19:49:01.536Z | 291.616° WNW | 43.62° | 2026-05-21 19:53:01.536Z | 145.8° SSE |
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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