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 53068U 26145.46068928 +.00000000 +00000-0 -95629-4 0 00002
2 53068 97.4460 326.5053 0001291 76.6529 283.4842 15.05661593 08
| Epoch (UTC): | 25 May 2026 11:03:23 |
| Eccentricity: | 0.0001291 |
| inclination: | 97.4460° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 326.5053° |
| argument of perigee: | 76.6529° |
| revolutions per day: | 15.05661593 |
| mean anomaly at epoch: | 283.4842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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