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 68968U 26145.50003470 +.00000000 +00000-0 -22854-1 0 00000
2 68968 53.1595 268.3152 0001017 50.2529 22.6888 15.65803227 09
| Epoch (UTC): | 25 May 2026 12:00:02 |
| Eccentricity: | 0.0001017 |
| inclination: | 53.1595° |
| perigee height: | 370 km |
| apogee height: | 372 km |
| right ascension of ascending node: | 268.3152° |
| argument of perigee: | 50.2529° |
| revolutions per day: | 15.65803227 |
| mean anomaly at epoch: | 22.6888° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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