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 68528U 26145.24983681 +.00000000 +00000-0 +73641-3 0 00005
2 68528 53.1578 133.8654 0000994 79.3072 280.8040 15.30203793 05
| Epoch (UTC): | 25 May 2026 05:59:45 |
| Eccentricity: | 0.0000994 |
| inclination: | 53.1578° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 133.8654° |
| argument of perigee: | 79.3072° |
| revolutions per day: | 15.30203793 |
| mean anomaly at epoch: | 280.8040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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