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 68676U 26145.37626637 +.00000000 +00000-0 +46731-3 0 00008
2 68676 97.2859 16.9967 0002019 86.5105 273.6369 15.33450381 09
| Epoch (UTC): | 25 May 2026 09:01:49 |
| Eccentricity: | 0.0002019 |
| inclination: | 97.2859° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 16.9967° |
| argument of perigee: | 86.5105° |
| revolutions per day: | 15.33450381 |
| mean anomaly at epoch: | 273.6369° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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