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 68535U 26145.36550497 +.00000000 +00000-0 +89868-3 0 00009
2 68535 53.1582 132.4648 0001186 90.1859 269.9283 15.42170312 04
| Epoch (UTC): | 25 May 2026 08:46:19 |
| Eccentricity: | 0.0001186 |
| inclination: | 53.1582° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 132.4648° |
| argument of perigee: | 90.1859° |
| revolutions per day: | 15.42170312 |
| mean anomaly at epoch: | 269.9283° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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