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 68729U 26145.58335647 +.00000000 +00000-0 -28117-1 0 00005
2 68729 97.2848 9.2238 0001703 98.5433 209.5692 15.57663514 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001703 |
| inclination: | 97.2848° |
| perigee height: | 393 km |
| apogee height: | 396 km |
| right ascension of ascending node: | 9.2238° |
| argument of perigee: | 98.5433° |
| revolutions per day: | 15.57663514 |
| mean anomaly at epoch: | 209.5692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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