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 68881U 26145.56002448 +.00000000 +00000-0 +63349-3 0 00009
2 68881 51.8713 352.1091 0007884 216.8232 143.2213 15.35330530 04
| Epoch (UTC): | 25 May 2026 13:26:26 |
| Eccentricity: | 0.0007884 |
| inclination: | 51.8713° |
| perigee height: | 455 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 352.1091° |
| argument of perigee: | 216.8232° |
| revolutions per day: | 15.35330530 |
| mean anomaly at epoch: | 143.2213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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