DECAYED
Showing default

HYPE, 62687 (Decayed)

Orbit data source: Space-Track

HYPE, 62687 was a payload satellite owned by AGH UST (PL) in LEO 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.

Not visible in the next 10 days
Identifier
62687, 2025-009CG
Orbit
Decayed
Country
Flag of PLPL / POL
Related business
Manufacturer
AGH UST
Mission
Decayed Amateur Technology
Bus & Motor
POCKETQUBE 1P, Unknown motor
Mass
0.25 kg wet, 0.25 kg dry
Launch date (UTC)
2025-01-14 (11 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.004 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 weeks ago

TLE from 2 weeks ago
0 HYPE
1 62687U 25009CG  25342.99077692  .17641269  25287-5  97681-3 0  9999
2 62687  97.3891  69.7424 0010293 277.6471  82.3660 16.41473001 50400
Epoch: 2025-12-08T23:46Z
TLE epoch observation values (Epoch: 2025-12-08T23:46:43.125Z)
Latitude
-0.00006°
Longitude
-4.91916°
Altitude
164.253 km
Speed
7.808 km/s
True Right ascension
04h 38m 58s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
00:39:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
165.421 km
Perigee altitude
151.964 km
Semi-major axis
6,536.829 km
Eccentricity
0.00103
Inclination
97.3891°
RAAN
69.7424°
Arg. of periapsis
277.6471°
True anomaly
82.48292°
Mean anomaly
82.366°
Eccentric anomaly
82.42446°
Mean motion
4.1067 °/min
Orbital period
87.66 mins
BSTAR
0.00097681
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|