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 68290U 26145.58335647 +.00000000 +00000-0 -80492-4 0 00005
2 68290 53.1600 321.1397 0000833 94.9434 36.4691 15.35404509 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000833 |
| inclination: | 53.1600° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 321.1397° |
| argument of perigee: | 94.9434° |
| revolutions per day: | 15.35404509 |
| mean anomaly at epoch: | 36.4691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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