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 68963U 26145.58335647 +.00000000 +00000-0 -21345-1 0 00001
2 68963 53.1595 267.9530 0001318 62.8525 98.2054 15.65520819 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001318 |
| inclination: | 53.1595° |
| perigee height: | 371 km |
| apogee height: | 373 km |
| right ascension of ascending node: | 267.9530° |
| argument of perigee: | 62.8525° |
| revolutions per day: | 15.65520819 |
| mean anomaly at epoch: | 98.2054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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