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 68181U 26145.35181227 +.00000000 +00000-0 +87047-3 0 00003
2 68181 53.1590 270.4406 0001168 86.7163 273.3975 15.38848092 03
| Epoch (UTC): | 25 May 2026 08:26:36 |
| Eccentricity: | 0.0001168 |
| inclination: | 53.1590° |
| perigee height: | 449 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 270.4406° |
| argument of perigee: | 86.7163° |
| revolutions per day: | 15.38848092 |
| mean anomaly at epoch: | 273.3975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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