ACS 3, 59588
Orbit data source: Space-Track
ACS 3, 59588 is a payload satellite owned by ARC (US) in SSO that was launched on Tue, 23 Apr 2024 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). 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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59588 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
ARC/NANAVU
Mission
Operational Civil Technology
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
16.1 kg wet, 16.1 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Sail, 7.0 m
Radar Cross Section
0.080 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 ACS 3
1 59588U 24077B 26317.67858175 .00030921 00000-0 20094-1 0 9992
2 59588 97.2839 204.4165 0097624 4.5710 355.6329 14.00061108128917Epoch: 2026-11-13T16:17Z
TLE epoch observation values (Epoch: 2026-11-13T16:17:09.463Z)
Latitude
0.00004°
Longitude
-92.66721°
Altitude
825.719 km
Speed
7.476 km/s
True Right ascension
13h 37m 39s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
01:04:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
961.668 km
Perigee altitude
819.745 km
Semi-major axis
7,268.843 km
Eccentricity
0.00976
Inclination
97.2839°
RAAN
204.4165°
Arg. of periapsis
4.571°
True anomaly
355.54667°
Mean anomaly
355.6329°
Eccentric anomaly
355.58989°
Mean motion
3.50223 °/min
Orbital period
102.79 mins
BSTAR
0.020094
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Other satellites on launch #77 in the year 2024 (2024-04-23 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.ACS 3 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-11-14 04:51:53.204Z | 23.668° NE | 2026-11-14 04:57:53.204Z | 108.272° ESE | 47.479° | 2026-11-14 05:02:53.204Z | 169.761° S |
| 7 mins | 2026-11-14 06:35:53.204Z | 334.366° NNW | 2026-11-14 06:38:53.204Z | 294.656° NW | 25.762° | 2026-11-14 06:42:53.204Z | 245.868° WSW |
| 8 mins | 2026-11-14 16:25:53.204Z | 154.245° SSE | 2026-11-14 16:28:53.204Z | 106.985° ESE | 67.298° | 2026-11-14 16:33:53.204Z | 354.229° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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