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 17528U 26017.93184808 +.00000000 +00000-0 +96513-4 0 00001
2 17528 97.4015 29.2773 0144646 172.7532 187.5806 14.54390734 08
| Epoch (UTC): | 17 January 2026 22:21:51 |
| Eccentricity: | 0.0144646 |
| inclination: | 97.4015° |
| perigee height: | 609 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 29.2773° |
| argument of perigee: | 172.7532° |
| revolutions per day: | 14.54390734 |
| mean anomaly at epoch: | 187.5806° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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