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PACE, 40022

Orbit data source: Space-Track

PACE, 40022 is a Taiwanese payload satellite in SSO that was launched on Thu, 19 Jun 2014 UTC via a DNEPR launch vehicle from the Orenburg, Russia (OREN). 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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Identifier
40022, 2014-033N
Orbit
SSO
Country
Flag of TWTW / TWN
Related business
Manufacturer
NCKU
Mission
Non-operational Commercial Technology
Bus & Motor
CUBESAT 2U, Unknown motor
Mass
2 kg wet, 2 kg dry
Launch date (UTC)
2014-06-19 (12 years ago)
Launch vehicle
DNEPR
Launch site
Orenburg, Russia (OREN)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.057 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 PACE
1 40022U 14033N   26032.95466483  .00005564  00000-0  35432-3 0  9997
2 40022  98.1210  29.6791 0005349 330.2883  29.8039 15.09202373632625
Epoch: 2026-02-01T22:54Z
TLE epoch observation values (Epoch: 2026-02-01T22:54:43.041Z)
Latitude
-0.00008°
Longitude
-86.15712°
Altitude
538.48 km
Speed
7.595 km/s
True Right ascension
01h 58m 42s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
16:05:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
539.346 km
Perigee altitude
531.95 km
Semi-major axis
6,913.785 km
Eccentricity
0.00053
Inclination
98.121°
RAAN
29.6791°
Arg. of periapsis
330.2883°
True anomaly
29.83438°
Mean anomaly
29.8039°
Eccentric anomaly
29.81914°
Mean motion
3.77546 °/min
Orbital period
95.35 mins
BSTAR
0.00035432
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