IHOPSAT-TD, 44859
Orbit data source: Space-Track
IHOPSAT-TD, 44859 is a payload satellite owned by Hera Systems (US) in LEO that was launched on Wed, 11 Dec 2019 UTC via a PSLV-QL launch vehicle from the Sirharikota (SRI). 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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44859 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Hera Systems
Mission
Operational Commercial Imaging
Bus & Motor
CUBESAT 12U, Unknown motor
Mass
22 kg wet, 22 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box, Unknown HBR
Radar Cross Section
0.080 m², Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 IHOPSAT-TD
1 44859U 19089H 25342.59578294 .00006237 00000-0 37683-3 0 9990
2 44859 36.9669 106.1360 0004681 110.7658 249.3589 15.10394556329143Epoch: 2025-12-08T14:17Z
TLE epoch observation values (Epoch: 2025-12-08T14:17:55.646Z)
Latitude
-0.00004°
Longitude
174.06154°
Altitude
535.258 km
Speed
7.597 km/s
True Right ascension
07h 04m 32s
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
22:06:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
541.153 km
Perigee altitude
534.679 km
Semi-major axis
6,916.053 km
Eccentricity
0.00047
Inclination
36.9669°
RAAN
106.136°
Arg. of periapsis
110.7658°
True anomaly
249.30871°
Mean anomaly
249.3589°
Eccentric anomaly
249.33381°
Mean motion
3.7736 °/min
Orbital period
95.4 mins
BSTAR
0.00037683
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Other satellites on launch #89 in the year 2019 (2019-12-11 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.IHOPSAT-TD 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-12-09 12:47:14.462Z | 221.047° SW | 2025-12-09 12:49:14.462Z | 173.657° S | 31.429° | 2025-12-09 12:52:14.462Z | 102.825° ESE |
| 6 mins | 2025-12-09 14:27:14.462Z | 252.809° W | 2025-12-09 14:30:14.462Z | 151.217° SSE | 38.4° | 2025-12-09 14:33:14.462Z | 103.953° ESE |
| 5 mins | 2025-12-09 16:08:14.462Z | 245.976° WSW | 2025-12-09 16:10:14.462Z | 190.852° SSW | 30.419° | 2025-12-09 16:13:14.462Z | 132.986° SE |
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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