View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 17590U 87027B 25114.71488765 .00000238 00000-0 14215-3 0 9994
2 17590 71.0031 228.6144 0007195 254.2244 105.8086 14.17107463970196
| Epoch (UTC): | 24 April 2025 17:09:26 |
| Eccentricity: | 0.0007195 |
| inclination: | 71.0031° |
| perigee height: | 830 km |
| apogee height: | 840 km |
| right ascension of ascending node: | 228.6144° |
| argument of perigee: | 254.2244° |
| revolutions per day: | 14.17107463 |
| mean anomaly at epoch: | 105.8086° |
| orbit number at epoch: | 97019 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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