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 68315U 26145.58335647 +.00000000 +00000-0 -59277-3 0 00009
2 68315 97.2843 271.8279 0001408 85.8922 81.5331 15.75220027 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001408 |
| inclination: | 97.2843° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.8279° |
| argument of perigee: | 85.8922° |
| revolutions per day: | 15.75220027 |
| mean anomaly at epoch: | 81.5331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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