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 68856U 26145.58335647 +.00000000 +00000-0 +18449-3 0 00004
2 68856 97.2847 160.3717 0001368 82.9200 1.0597 15.49178316 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001368 |
| inclination: | 97.2847° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 160.3717° |
| argument of perigee: | 82.9200° |
| revolutions per day: | 15.49178316 |
| mean anomaly at epoch: | 1.0597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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