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 57894U 26145.56099463 +.00000000 +00000-0 -44349-4 0 00005
2 57894 42.9994 239.9962 0001296 272.8951 87.1752 15.27560886 02
| Epoch (UTC): | 25 May 2026 13:27:49 |
| Eccentricity: | 0.0001296 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 239.9962° |
| argument of perigee: | 272.8951° |
| revolutions per day: | 15.27560886 |
| mean anomaly at epoch: | 87.1752° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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