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: 7 hours ago
TLE from 7 hours ago
0 HORACIO
1 59098U 24043A 25303.34926244 .00004363 00000-0 38423-3 0 9990
2 59098 97.8235 69.3291 0011795 71.5162 288.7340 14.96949498 90264Epoch: 2025-10-30T08:22Z
TLE epoch observation values (Epoch: 2025-10-30T08:22:56.274Z)
Latitude
-0.00007°
Longitude
-95.31469°
Altitude
576.749 km
Speed
7.574 km/s
True Right ascension
04h 37m 18s
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
10:56:24
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
581.542 km
Perigee altitude
565.144 km
Semi-major axis
6,951.48 km
Eccentricity
0.00118
Inclination
97.8235°
RAAN
69.3291°
Arg. of periapsis
71.5162°
True anomaly
288.60594°
Mean anomaly
288.734°
Eccentric anomaly
288.66998°
Mean motion
3.74479 °/min
Orbital period
96.13 mins
BSTAR
0.00038423
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-10-30 21:47:05.882Z | 355.747° N | 2025-10-30 21:50:05.882Z | 277.637° WNW | 36.816° | 2025-10-30 21:53:05.882Z | 215.225° SW |
| 6 mins | 2025-10-31 08:35:05.882Z | 168.742° S | 2025-10-31 08:37:05.882Z | 178.83° S | 43.593° | 2025-10-31 08:41:05.882Z | 346.559° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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