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 68814U 26145.55659854 +.00000000 +00000-0 +16399-2 0 00005
2 68814 97.2864 352.2331 0001109 108.4306 251.7080 15.75284464 06
| Epoch (UTC): | 25 May 2026 13:21:30 |
| Eccentricity: | 0.0001109 |
| inclination: | 97.2864° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 352.2331° |
| argument of perigee: | 108.4306° |
| revolutions per day: | 15.75284464 |
| mean anomaly at epoch: | 251.7080° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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