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 68682U 26145.35993692 +.00000000 +00000-0 -19545-3 0 00005
2 68682 97.2871 17.0192 0002645 86.2442 273.9103 15.33445809 06
| Epoch (UTC): | 25 May 2026 08:38:18 |
| Eccentricity: | 0.0002645 |
| inclination: | 97.2871° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 17.0192° |
| argument of perigee: | 86.2442° |
| revolutions per day: | 15.33445809 |
| mean anomaly at epoch: | 273.9103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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