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 68889U 26145.58335647 +.00000000 +00000-0 -46918-1 0 00001
2 68889 51.8862 351.9663 0003534 205.3522 285.8243 15.26358074 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0003534 |
| inclination: | 51.8862° |
| perigee height: | 484 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 351.9663° |
| argument of perigee: | 205.3522° |
| revolutions per day: | 15.26358074 |
| mean anomaly at epoch: | 285.8243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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