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 68275U 26144.78293455 +.00000000 +00000-0 +63715-3 0 00006
2 68275 53.1594 324.9313 0000697 84.1648 275.9435 15.35406596 04
| Epoch (UTC): | 24 May 2026 18:47:25 |
| Eccentricity: | 0.0000697 |
| inclination: | 53.1594° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 324.9313° |
| argument of perigee: | 84.1648° |
| revolutions per day: | 15.35406596 |
| mean anomaly at epoch: | 275.9435° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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