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 68045U 26145.12094590 +.00000000 +00000-0 +82510-3 0 00003
2 68045 53.1593 53.2101 0001186 86.2825 273.8313 15.34400398 04
| Epoch (UTC): | 25 May 2026 02:54:09 |
| Eccentricity: | 0.0001186 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 53.2101° |
| argument of perigee: | 86.2825° |
| revolutions per day: | 15.34400398 |
| mean anomaly at epoch: | 273.8313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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