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 68274U 26145.50375763 +.00000000 +00000-0 +10225-2 0 00006
2 68274 53.1593 321.6091 0000576 52.5517 307.5538 15.34411866 00
| Epoch (UTC): | 25 May 2026 12:05:24 |
| Eccentricity: | 0.0000576 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 321.6091° |
| argument of perigee: | 52.5517° |
| revolutions per day: | 15.34411866 |
| mean anomaly at epoch: | 307.5538° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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