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 26162.25995573 +.00000000 +00000-0 +13295-3 0 00001
2 17528 97.4031 157.1598 0145574 77.9076 283.8392 14.54606052 05
| Epoch (UTC): | 11 June 2026 06:14:20 |
| Eccentricity: | 0.0145574 |
| inclination: | 97.4031° |
| perigee height: | 607 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 157.1598° |
| argument of perigee: | 77.9076° |
| revolutions per day: | 14.54606052 |
| mean anomaly at epoch: | 283.8392° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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