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 68570U 26145.60758593 +.00000000 +00000-0 +10066-2 0 00005
2 68570 53.1609 5.1482 0001512 90.2850 269.8326 15.34412749 01
| Epoch (UTC): | 25 May 2026 14:34:55 |
| Eccentricity: | 0.0001512 |
| inclination: | 53.1609° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 5.1482° |
| argument of perigee: | 90.2850° |
| revolutions per day: | 15.34412749 |
| mean anomaly at epoch: | 269.8326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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