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 68207U 26145.22777625 +.00000000 +00000-0 +47607-3 0 00009
2 68207 97.2882 20.6122 0001889 98.9942 261.1515 15.33442883 03
| Epoch (UTC): | 25 May 2026 05:27:59 |
| Eccentricity: | 0.0001889 |
| inclination: | 97.2882° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 20.6122° |
| argument of perigee: | 98.9942° |
| revolutions per day: | 15.33442883 |
| mean anomaly at epoch: | 261.1515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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