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 68960U 26145.58335647 +.00000000 +00000-0 +48933-3 0 00001
2 68960 53.1587 268.8247 0001843 40.1720 52.1491 15.49324915 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001843 |
| inclination: | 53.1587° |
| perigee height: | 417 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 268.8247° |
| argument of perigee: | 40.1720° |
| revolutions per day: | 15.49324915 |
| mean anomaly at epoch: | 52.1491° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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