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 68940U 26145.37677676 +.00000000 +00000-0 +40469-3 0 00003
2 68940 51.8731 177.6275 0006102 69.4908 290.6731 15.34136040 09
| Epoch (UTC): | 25 May 2026 09:02:33 |
| Eccentricity: | 0.0006102 |
| inclination: | 51.8731° |
| perigee height: | 459 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 177.6275° |
| argument of perigee: | 69.4908° |
| revolutions per day: | 15.34136040 |
| mean anomaly at epoch: | 290.6731° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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