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 54255U 26145.63212288 +.00000000 +00000-0 +54700-3 0 00003
2 54255 97.6165 287.1969 0004898 102.2761 257.9042 15.57586391 06
| Epoch (UTC): | 25 May 2026 15:10:15 |
| Eccentricity: | 0.0004898 |
| inclination: | 97.6165° |
| perigee height: | 391 km |
| apogee height: | 398 km |
| right ascension of ascending node: | 287.1969° |
| argument of perigee: | 102.2761° |
| revolutions per day: | 15.57586391 |
| mean anomaly at epoch: | 257.9042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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