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: 1 day ago
TLE from 1 day ago
0 STPSAT-7
1 68630U 26074D 26143.83506977 .00004576 00000-0 19552-3 0 9990
2 68630 60.0215 271.5936 0023410 6.9930 353.1472 15.24381951 7066Epoch: 2026-05-23T20:02Z
TLE epoch observation values (Epoch: 2026-05-23T20:02:30.028Z)
Latitude
-0.00004°
Longitude
89.52259°
Altitude
478.273 km
Speed
7.636 km/s
True Right ascension
18h 06m 22s
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
09:38:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
507.924 km
Perigee altitude
475.759 km
Semi-major axis
6,869.979 km
Eccentricity
0.00234
Inclination
60.0215°
RAAN
271.5936°
Arg. of periapsis
6.993°
True anomaly
353.1151°
Mean anomaly
353.1472°
Eccentric anomaly
353.13116°
Mean motion
3.81162 °/min
Orbital period
94.45 mins
BSTAR
0.00019552
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-05-25 09:58:22.582Z | 193.084° SSW | 2026-05-25 10:01:22.582Z | 101.824° ESE | 34.784° | 2026-05-25 10:04:22.582Z | 50.929° ENE |
| 4 mins | 2026-05-25 11:37:22.582Z | 293.102° NW | 2026-05-25 11:38:22.582Z | 312.583° NW | 17.119° | 2026-05-25 11:41:22.582Z | 6.738° NNE |
| 7 mins | 2026-05-25 18:12:22.582Z | 327.639° NNW | 2026-05-25 18:15:22.582Z | 20.568° NNE | 41.567° | 2026-05-25 18:19:22.582Z | 132.346° SE |
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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