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 68568U 26145.60968955 +.00000000 +00000-0 +90923-3 0 00008
2 68568 53.1591 5.1520 0001853 87.0017 273.1197 15.34409905 02
| Epoch (UTC): | 25 May 2026 14:37:57 |
| Eccentricity: | 0.0001853 |
| inclination: | 53.1591° |
| perigee height: | 461 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 5.1520° |
| argument of perigee: | 87.0017° |
| revolutions per day: | 15.34409905 |
| mean anomaly at epoch: | 273.1197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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