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 is defined by the following mean orbital elements,
1 59588U 26019.28104213 +.00000000 +00000-0 +54121-2 0 00002
2 59588 97.2377 331.4922 0054631 240.4023 119.1690 13.87302153 00
| Epoch (UTC): | 19 January 2026 06:44:42 |
| Eccentricity: | 0.0054631 |
| inclination: | 97.2377° |
| perigee height: | 898 km |
| apogee height: | 978 km |
| right ascension of ascending node: | 331.4922° |
| argument of perigee: | 240.4023° |
| revolutions per day: | 13.87302153 |
| mean anomaly at epoch: | 119.1690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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