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 68882U 26145.58335647 +.00000000 +00000-0 -12770+0 0 00001
2 68882 51.8875 352.6183 0005082 220.1911 4.6786 15.15480930 04
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0005082 |
| inclination: | 51.8875° |
| perigee height: | 516 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 352.6183° |
| argument of perigee: | 220.1911° |
| revolutions per day: | 15.15480930 |
| mean anomaly at epoch: | 4.6786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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