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 68063U 26145.46766824 +.00000000 +00000-0 +60517-3 0 00009
2 68063 53.1604 51.8111 0001856 102.5797 257.5413 15.34400892 05
| Epoch (UTC): | 25 May 2026 11:13:26 |
| Eccentricity: | 0.0001856 |
| inclination: | 53.1604° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 51.8111° |
| argument of perigee: | 102.5797° |
| revolutions per day: | 15.34400892 |
| mean anomaly at epoch: | 257.5413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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