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 26069.52934264 +.00000000 +00000-0 +26242-3 0 00003
2 17528 97.4037 74.9775 0144559 11.0988 349.3342 14.54488208 01
| Epoch (UTC): | 10 March 2026 12:42:15 |
| Eccentricity: | 0.0144559 |
| inclination: | 97.4037° |
| perigee height: | 609 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 74.9775° |
| argument of perigee: | 11.0988° |
| revolutions per day: | 14.54488208 |
| mean anomaly at epoch: | 349.3342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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