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 68766U 26145.58335647 +.00000000 +00000-0 -53160-1 0 00002
2 68766 97.2855 182.3502 0001946 115.5773 170.1902 15.51453983 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001946 |
| inclination: | 97.2855° |
| perigee height: | 411 km |
| apogee height: | 414 km |
| right ascension of ascending node: | 182.3502° |
| argument of perigee: | 115.5773° |
| revolutions per day: | 15.51453983 |
| mean anomaly at epoch: | 170.1902° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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