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 68962U 26145.58335647 +.00000000 +00000-0 -21494-1 0 00005
2 68962 53.1594 267.9677 0001335 63.1370 90.4271 15.65276017 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001335 |
| inclination: | 53.1594° |
| perigee height: | 372 km |
| apogee height: | 373 km |
| right ascension of ascending node: | 267.9677° |
| argument of perigee: | 63.1370° |
| revolutions per day: | 15.65276017 |
| mean anomaly at epoch: | 90.4271° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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