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 68395U 26145.37652745 +.00000000 +00000-0 +63549-3 0 00001
2 68395 97.2841 287.8766 0001248 82.6213 277.5172 15.33454217 01
| Epoch (UTC): | 25 May 2026 09:02:11 |
| Eccentricity: | 0.0001248 |
| inclination: | 97.2841° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 287.8766° |
| argument of perigee: | 82.6213° |
| revolutions per day: | 15.33454217 |
| mean anomaly at epoch: | 277.5172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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