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 68819U 26145.55201213 +.00000000 +00000-0 +17652-2 0 00005
2 68819 97.2858 352.2373 0001615 86.3237 273.8213 15.75298241 00
| Epoch (UTC): | 25 May 2026 13:14:53 |
| Eccentricity: | 0.0001615 |
| inclination: | 97.2858° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 352.2373° |
| argument of perigee: | 86.3237° |
| revolutions per day: | 15.75298241 |
| mean anomaly at epoch: | 273.8213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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