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 68206U 26145.46898152 +.00000000 +00000-0 +18031-2 0 00001
2 68206 97.3343 215.5220 0507699 143.4665 220.2338 14.77427378 05
| Epoch (UTC): | 25 May 2026 11:15:20 |
| Eccentricity: | 0.0507699 |
| inclination: | 97.3343° |
| perigee height: | 281 km |
| apogee height: | 994 km |
| right ascension of ascending node: | 215.5220° |
| argument of perigee: | 143.4665° |
| revolutions per day: | 14.77427378 |
| mean anomaly at epoch: | 220.2338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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