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 68969U 26145.58335647 +.00000000 +00000-0 -10486-1 0 00001
2 68969 53.1595 267.8178 0001189 68.4602 158.5598 15.70963452 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001189 |
| inclination: | 53.1595° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 267.8178° |
| argument of perigee: | 68.4602° |
| revolutions per day: | 15.70963452 |
| mean anomaly at epoch: | 158.5598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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