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 68820U 26145.58335647 +.00000000 +00000-0 -59991-3 0 00003
2 68820 97.2844 352.2796 0001369 81.6825 114.0645 15.75232070 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001369 |
| inclination: | 97.2844° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 352.2796° |
| argument of perigee: | 81.6825° |
| revolutions per day: | 15.75232070 |
| mean anomaly at epoch: | 114.0645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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