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 54055U 26145.01175713 +.00000000 +00000-0 -30930-3 0 00004
2 54055 53.2155 1.6663 0001856 97.3591 262.7612 15.08868348 05
| Epoch (UTC): | 25 May 2026 00:16:55 |
| Eccentricity: | 0.0001856 |
| inclination: | 53.2155° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 1.6663° |
| argument of perigee: | 97.3591° |
| revolutions per day: | 15.08868348 |
| mean anomaly at epoch: | 262.7612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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