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 68425U 26145.38931833 +.00000000 +00000-0 +22885-3 0 00002
2 68425 97.4572 104.2464 0003365 72.6406 287.5196 15.18523819 05
| Epoch (UTC): | 25 May 2026 09:20:37 |
| Eccentricity: | 0.0003365 |
| inclination: | 97.4572° |
| perigee height: | 508 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 104.2464° |
| argument of perigee: | 72.6406° |
| revolutions per day: | 15.18523819 |
| mean anomaly at epoch: | 287.5196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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