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 68546U 26145.33652051 +.00000000 +00000-0 +64422-3 0 00006
2 68546 53.1605 6.2832 0001151 80.4120 279.7012 15.34402935 09
| Epoch (UTC): | 25 May 2026 08:04:35 |
| Eccentricity: | 0.0001151 |
| inclination: | 53.1605° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 6.2832° |
| argument of perigee: | 80.4120° |
| revolutions per day: | 15.34402935 |
| mean anomaly at epoch: | 279.7012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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