Showing default

PACE-1, 48909

Orbit data source: Space-Track

PACE-1, 48909 is a payload satellite owned by ARC (US) in SSO that was launched on Wed, 30 Jun 2021 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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
48909, 2021-059AG
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
ARC
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 6U, Unknown motor
Mass
10 kg wet, 10 kg dry
Launch date (UTC)
2021-06-30 (4 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.1 m
Radar Cross Section
0.080 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 PACE-1
1 48909U 21059AG  25355.75676501  .00033955  00000-0  44722-3 0  9991
2 48909  97.6817 172.0800 0002548 243.2222 116.8773 15.58376238249998
Epoch: 2025-12-21T18:09Z
TLE epoch observation values (Epoch: 2025-12-21T18:09:44.496Z)
Latitude
-0°
Longitude
169.07996°
Altitude
396.27 km
Speed
7.672 km/s
True Right ascension
11h 28m 19s
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
05:51:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
391.007 km
Perigee altitude
387.559 km
Semi-major axis
6,767.42 km
Eccentricity
0.00025
Inclination
97.6817°
RAAN
172.08°
Arg. of periapsis
243.2222°
True anomaly
116.90334°
Mean anomaly
116.8773°
Eccentric anomaly
116.89032°
Mean motion
3.8986 °/min
Orbital period
92.34 mins
BSTAR
0.00044722
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|