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 68017U 26145.38644031 +.00000000 +00000-0 +36551-3 0 00005
2 68017 97.2848 94.3499 0001825 97.8570 262.2880 15.33442299 02
| Epoch (UTC): | 25 May 2026 09:16:28 |
| Eccentricity: | 0.0001825 |
| inclination: | 97.2848° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.3499° |
| argument of perigee: | 97.8570° |
| revolutions per day: | 15.33442299 |
| mean anomaly at epoch: | 262.2880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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