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 68711U 26145.58335647 +.00000000 +00000-0 -42451-1 0 00003
2 68711 53.1597 37.2375 0001282 108.1542 167.0514 15.45116419 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001282 |
| inclination: | 53.1597° |
| perigee height: | 430 km |
| apogee height: | 432 km |
| right ascension of ascending node: | 37.2375° |
| argument of perigee: | 108.1542° |
| revolutions per day: | 15.45116419 |
| mean anomaly at epoch: | 167.0514° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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