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 54157U 26145.10193782 +.00000000 +00000-0 -76704-4 0 00003
2 54157 53.2159 31.0403 0001356 88.1801 271.9346 15.08833869 04
| Epoch (UTC): | 25 May 2026 02:26:47 |
| Eccentricity: | 0.0001356 |
| inclination: | 53.2159° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 31.0403° |
| argument of perigee: | 88.1801° |
| revolutions per day: | 15.08833869 |
| mean anomaly at epoch: | 271.9346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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