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 68773U 26145.58335647 +.00000000 +00000-0 +12317-2 0 00009
2 68773 97.2855 182.3356 0001271 92.8105 168.2622 15.49152860 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001271 |
| inclination: | 97.2855° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 182.3356° |
| argument of perigee: | 92.8105° |
| revolutions per day: | 15.49152860 |
| mean anomaly at epoch: | 168.2622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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