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 54190U 26145.64382542 +.00000000 +00000-0 -11946-3 0 00009
2 54190 53.2114 8.7775 0001055 91.7239 268.3874 15.08818072 01
| Epoch (UTC): | 25 May 2026 15:27:06 |
| Eccentricity: | 0.0001055 |
| inclination: | 53.2114° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 8.7775° |
| argument of perigee: | 91.7239° |
| revolutions per day: | 15.08818072 |
| mean anomaly at epoch: | 268.3874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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