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 68600U 26145.40766250 +.00000000 +00000-0 +81911-3 0 00004
2 68600 51.8700 287.2299 0008848 297.8336 62.1754 15.37618273 06
| Epoch (UTC): | 25 May 2026 09:47:02 |
| Eccentricity: | 0.0008848 |
| inclination: | 51.8700° |
| perigee height: | 447 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 287.2299° |
| argument of perigee: | 297.8336° |
| revolutions per day: | 15.37618273 |
| mean anomaly at epoch: | 62.1754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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