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 68797U 26145.40494453 +.00000000 +00000-0 +37720-3 0 00003
2 68797 97.5036 295.3211 0016598 151.7648 208.4483 15.08327750 00
| Epoch (UTC): | 25 May 2026 09:43:07 |
| Eccentricity: | 0.0016598 |
| inclination: | 97.5036° |
| perigee height: | 530 km |
| apogee height: | 553 km |
| right ascension of ascending node: | 295.3211° |
| argument of perigee: | 151.7648° |
| revolutions per day: | 15.08327750 |
| mean anomaly at epoch: | 208.4483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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