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 68323U 26145.58335647 +.00000000 +00000-0 +71232-3 0 00002
2 68323 53.1603 346.9418 0001371 115.5794 359.6912 15.35377879 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001371 |
| inclination: | 53.1603° |
| perigee height: | 459 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 346.9418° |
| argument of perigee: | 115.5794° |
| revolutions per day: | 15.35377879 |
| mean anomaly at epoch: | 359.6912° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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