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.

Loading next visibility...
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 (5 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: 11 hours ago

TLE from 11 hours ago
0 PACE-1
1 48909U 21059AG  26094.99974342  .00071915  00000-0  59805-3 0  9998
2 48909  97.6839 285.4883 0002912 208.1235 151.9869 15.69924511266283
Epoch: 2026-04-04T23:59Z
TLE epoch observation values (Epoch: 2026-04-04T23:59:37.831Z)
Latitude
-0.00006°
Longitude
92.26922°
Altitude
363.995 km
Speed
7.69 km/s
True Right ascension
19h 01m 57s
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
17:06:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
357.986 km
Perigee altitude
354.064 km
Semi-major axis
6,734.162 km
Eccentricity
0.00029
Inclination
97.6839°
RAAN
285.4883°
Arg. of periapsis
208.1235°
True anomaly
152.00257°
Mean anomaly
151.9869°
Eccentric anomaly
151.99473°
Mean motion
3.92751 °/min
Orbital period
91.66 mins
BSTAR
0.00059805
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|