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 68245U 26145.42508988 +.00000000 +00000-0 +97591-3 0 00004
2 68245 53.1566 296.6721 0001007 92.7690 267.3434 15.49352378 03
| Epoch (UTC): | 25 May 2026 10:12:07 |
| Eccentricity: | 0.0001007 |
| inclination: | 53.1566° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 296.6721° |
| argument of perigee: | 92.7690° |
| revolutions per day: | 15.49352378 |
| mean anomaly at epoch: | 267.3434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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