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 68677U 26145.58018916 +.00000000 +00000-0 +45108-3 0 00004
2 68677 97.2854 17.1772 0002327 103.0304 257.1199 15.33453765 07
| Epoch (UTC): | 25 May 2026 13:55:28 |
| Eccentricity: | 0.0002327 |
| inclination: | 97.2854° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 17.1772° |
| argument of perigee: | 103.0304° |
| revolutions per day: | 15.33453765 |
| mean anomaly at epoch: | 257.1199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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