HORACIO, 59098
Orbit data source: Space-Track
HORACIO, 59098 is a payload satellite owned by Satlantis (ES) in SSO that was launched on Mon, 04 Mar 2024 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.
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59098 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
ES / SPNRelated business
Manufacturer
NanoAvionics
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 16U M16P, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, 0.2 m
Radar Cross Section
0.100 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 HORACIO
1 59098U 24043A 25260.96450795 .00003319 00000-0 29687-3 0 9995
2 59098 97.8180 26.9476 0010706 202.5778 157.4973 14.96525207 83924Epoch: 2025-09-17T23:08Z
TLE epoch observation values (Epoch: 2025-09-17T23:08:53.486Z)
Latitude
-0.0001°
Longitude
42.59185°
Altitude
587.572 km
Speed
7.563 km/s
True Right ascension
01h 47m 47s
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
00:18:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
582.101 km
Perigee altitude
567.214 km
Semi-major axis
6,952.795 km
Eccentricity
0.00107
Inclination
97.818°
RAAN
26.9476°
Arg. of periapsis
202.5778°
True anomaly
157.5442°
Mean anomaly
157.4973°
Eccentric anomaly
157.52075°
Mean motion
3.74373 °/min
Orbital period
96.16 mins
BSTAR
0.00029687
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Other satellites on launch #43 in the year 2024 (2024-03-04 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.HORACIO 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-09-18 08:53:53.521Z | 190.147° SSW | 2025-09-18 08:56:53.521Z | 249.121° W | 35.397° | 2025-09-18 09:00:53.521Z | 333.965° NNW |
| 4 mins | 2025-09-18 20:36:53.521Z | 64.777° ENE | 2025-09-18 20:37:53.521Z | 85.585° E | 21.696° | 2025-09-18 20:40:53.521Z | 143.121° SSE |
| 4 mins | 2025-09-18 22:11:53.521Z | 325.334° NNW | 2025-09-18 22:13:53.521Z | 280.99° WNW | 22.44° | 2025-09-18 22:15:53.521Z | 244.775° WSW |
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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