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 68884U 26145.58335647 +.00000000 +00000-0 -72422-2 0 00006
2 68884 51.8828 352.0676 0006515 215.9866 257.2036 15.27288312 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0006515 |
| inclination: | 51.8828° |
| perigee height: | 479 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 352.0676° |
| argument of perigee: | 215.9866° |
| revolutions per day: | 15.27288312 |
| mean anomaly at epoch: | 257.2036° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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