HYPE, 62687
Orbit data source: Space-Track
HYPE, 62687 is a payload satellite owned by AGH UST (PL) in SSO that was launched on Tue, 14 Jan 2025 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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62687 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
PL / POLRelated business
Manufacturer
AGH UST
Mission
Operational Amateur Technology
Bus & Motor
POCKETQUBE 1P, Unknown motor
Mass
0.25 kg wet, 0.25 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.004 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 HYPE
1 62687U 25009CG 25298.22283698 .00216817 00000-0 30733-2 0 9994
2 62687 97.4265 22.0211 0003887 280.6408 79.4408 15.55702080 43367Epoch: 2025-10-25T05:20Z
TLE epoch observation values (Epoch: 2025-10-25T05:20:53.115Z)
Latitude
-0.00005°
Longitude
-92.05668°
Altitude
402.769 km
Speed
7.669 km/s
True Right ascension
01h 28m 05s
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
20:07:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
399.665 km
Perigee altitude
394.398 km
Semi-major axis
6,775.169 km
Eccentricity
0.00039
Inclination
97.4265°
RAAN
22.0211°
Arg. of periapsis
280.6408°
True anomaly
79.48459°
Mean anomaly
79.4408°
Eccentric anomaly
79.4627°
Mean motion
3.89191 °/min
Orbital period
92.5 mins
BSTAR
0.0030733
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Other satellites on launch #9 in the year 2025 (2025-01-14 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.HYPE 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-26 06:10:49.793Z | 202.279° SSW | 2025-10-26 06:12:49.793Z | 263.973° W | 29.604° | 2025-10-26 06:14:49.793Z | 321.886° NNW |
| 4 mins | 2025-10-26 18:57:49.793Z | 336.649° NNW | 2025-10-26 18:58:49.793Z | 298.156° NW | 32.391° | 2025-10-26 19:01:49.793Z | 215.435° SW |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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