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 68597U 26145.58335647 +.00000000 +00000-0 -85380-1 0 00003
2 68597 51.8778 286.9941 0008384 303.6642 26.5625 15.25245496 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0008384 |
| inclination: | 51.8778° |
| perigee height: | 484 km |
| apogee height: | 496 km |
| right ascension of ascending node: | 286.9941° |
| argument of perigee: | 303.6642° |
| revolutions per day: | 15.25245496 |
| mean anomaly at epoch: | 26.5625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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