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 68798U 26145.39830313 +.00000000 +00000-0 +21651-3 0 00007
2 68798 97.5040 295.3339 0019966 155.2834 204.9356 15.08580463 07
| Epoch (UTC): | 25 May 2026 09:33:33 |
| Eccentricity: | 0.0019966 |
| inclination: | 97.5040° |
| perigee height: | 527 km |
| apogee height: | 554 km |
| right ascension of ascending node: | 295.3339° |
| argument of perigee: | 155.2834° |
| revolutions per day: | 15.08580463 |
| mean anomaly at epoch: | 204.9356° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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