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 68785U 26145.58335647 +.00000000 +00000-0 -20008-1 0 00008
2 68785 97.2851 182.4907 0001451 105.7560 159.7715 15.67338730 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001451 |
| inclination: | 97.2851° |
| perigee height: | 366 km |
| apogee height: | 368 km |
| right ascension of ascending node: | 182.4907° |
| argument of perigee: | 105.7560° |
| revolutions per day: | 15.67338730 |
| mean anomaly at epoch: | 159.7715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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