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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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: 17 hours ago
TLE from 17 hours ago
0 IHOPSAT-TD
1 44859U 19089H 26083.00395896 .00003663 00000-0 21786-3 0 9991
2 44859 36.9664 191.6963 0005948 258.3364 101.6714 15.11324474345091Epoch: 2026-03-24T00:05Z
TLE epoch observation values (Epoch: 2026-03-24T00:05:42.054Z)
Latitude
-0.00001°
Longitude
8.78322°
Altitude
532.113 km
Speed
7.598 km/s
True Right ascension
12h 46m 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
22:34:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
539.193 km
Perigee altitude
530.969 km
Semi-major axis
6,913.218 km
Eccentricity
0.00059
Inclination
36.9664°
RAAN
191.6963°
Arg. of periapsis
258.3364°
True anomaly
101.73814°
Mean anomaly
101.6714°
Eccentric anomaly
101.70477°
Mean motion
3.77592 °/min
Orbital period
95.34 mins
BSTAR
0.00021786
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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 | 2026-03-25 11:15:19.630Z | 216.403° SW | 2026-03-25 11:17:19.630Z | 163.916° S | 31.094° | 2026-03-25 11:20:19.630Z | 101.166° ESE |
| 6 mins | 2026-03-25 12:55:19.630Z | 250.014° W | 2026-03-25 12:57:19.630Z | 197° SSW | 39.412° | 2026-03-25 13:01:19.630Z | 102.332° ESE |
| 6 mins | 2026-03-25 14:35:19.630Z | 254.488° W | 2026-03-25 14:37:19.630Z | 214.038° SW | 30.373° | 2026-03-25 14:41:19.630Z | 129.333° 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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