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 54159U 26145.38068992 +.00000000 +00000-0 -40592-4 0 00005
2 54159 53.2136 29.9396 0001203 72.5589 287.5535 15.08827427 05
| Epoch (UTC): | 25 May 2026 09:08:11 |
| Eccentricity: | 0.0001203 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 29.9396° |
| argument of perigee: | 72.5589° |
| revolutions per day: | 15.08827427 |
| mean anomaly at epoch: | 287.5535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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