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 35682U 26145.36505544 +.00000000 +00000-0 +13057-3 0 00006
2 35682 98.0021 278.8776 0011315 139.0267 221.1794 14.75079288 07
| Epoch (UTC): | 25 May 2026 08:45:40 |
| Eccentricity: | 0.0011315 |
| inclination: | 98.0021° |
| perigee height: | 637 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 278.8776° |
| argument of perigee: | 139.0267° |
| revolutions per day: | 14.75079288 |
| mean anomaly at epoch: | 221.1794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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