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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 (11 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: 16 hours ago

TLE from 16 hours ago
0 PACE
1 40022U 14033N   25348.94462450  .00004042  00000-0  26410-3 0  9991
2 40022  98.1177 337.8668 0007921 114.1071 246.0985 15.08423730625233
Epoch: 2025-12-14T22:40Z
TLE epoch observation values (Epoch: 2025-12-14T22:40:15.556Z)
Latitude
-0.00005°
Longitude
-86.04828°
Altitude
546.294 km
Speed
7.588 km/s
True Right ascension
22h 31m 28s
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
13:24:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
543.507 km
Perigee altitude
532.551 km
Semi-major axis
6,916.166 km
Eccentricity
0.00079
Inclination
98.1177°
RAAN
337.8668°
Arg. of periapsis
114.1071°
True anomaly
246.01555°
Mean anomaly
246.0985°
Eccentric anomaly
246.05702°
Mean motion
3.77351 °/min
Orbital period
95.4 mins
BSTAR
0.0002641
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Documentation

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