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 68517U 26145.34878809 +.00000000 +00000-0 +98827-3 0 00002
2 68517 53.1587 133.0882 0001243 70.9428 289.1712 15.42172494 02
| Epoch (UTC): | 25 May 2026 08:22:15 |
| Eccentricity: | 0.0001243 |
| inclination: | 53.1587° |
| perigee height: | 439 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 133.0882° |
| argument of perigee: | 70.9428° |
| revolutions per day: | 15.42172494 |
| mean anomaly at epoch: | 289.1712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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