DECAYED
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IT'S ABOUT TIME, 56189 (Decayed)

Orbit data source: Space-Track

IT'S ABOUT TIME, 56189 was a payload satellite owned by TrustPoint (US) in LEO that was launched on Sat, 15 Apr 2023 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
56189, 2023-054M
Orbit
Decayed
Country
Flag of USUS
Related business
Manufacturer
TrustPoint
Mission
Decayed Commercial Navigation
Bus & Motor
CUBESAT 3U?, Unknown motor
Mass
4 kg wet, 4 kg dry
Launch date (UTC)
2023-04-15 (2 years 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
0.035 m², Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 month ago

TLE from 1 month ago
0 IT'S ABOUT TIME
1 56189U 23054M   25212.82742210  .08308457  25724-5  68337-3 0  9991
2 56189  97.2931 127.4768 0007009 204.4693 155.6275 16.39847219129790
Epoch: 2025-07-31T19:51Z
TLE epoch observation values (Epoch: 2025-07-31T19:51:29.269Z)
Latitude
-0.00002°
Longitude
-120.08186°
Altitude
173.643 km
Speed
7.799 km/s
True Right ascension
08h 29m 54s
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
11:11:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
167.597 km
Perigee altitude
158.427 km
Semi-major axis
6,541.149 km
Eccentricity
0.0007
Inclination
97.2931°
RAAN
127.4768°
Arg. of periapsis
204.4693°
True anomaly
155.66062°
Mean anomaly
155.6275°
Eccentric anomaly
155.64406°
Mean motion
4.10263 °/min
Orbital period
87.75 mins
BSTAR
0.00068337
Loading maneuver chart data...
Computing Atmospheric mass density...

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