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, 6.3 m
Radar Cross Section
0.080 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 ACS 3
1 59588U 24077B 26047.82550737 .00016079 00000-0 13219-1 0 9991
2 59588 97.2185 353.6281 0047656 138.6275 221.8513 13.88698762 91300Epoch: 2026-02-16T19:48Z
TLE epoch observation values (Epoch: 2026-02-16T19:48:43.836Z)
Latitude
-0.00008°
Longitude
-90.36884°
Altitude
962.142 km
Speed
7.358 km/s
True Right ascension
23h 34m 30s
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
08:36:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
965.16 km
Perigee altitude
895.501 km
Semi-major axis
7,308.468 km
Eccentricity
0.00477
Inclination
97.2185°
RAAN
353.6281°
Arg. of periapsis
138.6275°
True anomaly
221.48856°
Mean anomaly
221.8513°
Eccentric anomaly
221.66977°
Mean motion
3.47379 °/min
Orbital period
103.63 mins
BSTAR
0.013219
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-02-17 08:31:01.008Z | 29.288° NE | 2026-02-17 08:35:01.008Z | 84.265° E | 34.481° | 2026-02-17 08:40:01.008Z | 164.893° S |
| 7 mins | 2026-02-17 10:15:01.008Z | 331.927° NNW | 2026-02-17 10:18:01.008Z | 288.983° WNW | 23.095° | 2026-02-17 10:22:01.008Z | 242.037° WSW |
| 9 mins | 2026-02-17 20:09:01.008Z | 158.15° S | 2026-02-17 20:13:01.008Z | 75.616° E | 44.146° | 2026-02-17 20:18:01.008Z | 352.56° N |
| 4 mins | 2026-02-17 21:55:01.008Z | 259.312° W | 2026-02-17 21:56:01.008Z | 270.499° WNW | 14.061° | 2026-02-17 21:59:01.008Z | 302.125° NW |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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