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 68769U 26145.58335647 +.00000000 +00000-0 +12031-2 0 00007
2 68769 97.2853 182.3145 0000748 116.6209 95.1436 15.49156817 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000748 |
| inclination: | 97.2853° |
| perigee height: | 419 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 182.3145° |
| argument of perigee: | 116.6209° |
| revolutions per day: | 15.49156817 |
| mean anomaly at epoch: | 95.1436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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