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 68567U 26145.02757631 +.00000000 +00000-0 +67914-3 0 00004
2 68567 53.1592 7.1805 0001020 99.0526 261.0592 15.34417667 03
| Epoch (UTC): | 25 May 2026 00:39:42 |
| Eccentricity: | 0.0001020 |
| inclination: | 53.1592° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 7.1805° |
| argument of perigee: | 99.0526° |
| revolutions per day: | 15.34417667 |
| mean anomaly at epoch: | 261.0592° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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