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 68026U 26145.36741238 +.00000000 +00000-0 +64435-3 0 00002
2 68026 97.2847 94.3757 0002875 81.4916 278.6652 15.33446711 08
| Epoch (UTC): | 25 May 2026 08:49:04 |
| Eccentricity: | 0.0002875 |
| inclination: | 97.2847° |
| perigee height: | 464 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 94.3757° |
| argument of perigee: | 81.4916° |
| revolutions per day: | 15.33446711 |
| mean anomaly at epoch: | 278.6652° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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