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 54195U 26145.04395366 +.00000000 +00000-0 +26159-4 0 00008
2 54195 53.2144 11.4324 0001470 77.3561 282.7596 15.08841338 01
| Epoch (UTC): | 25 May 2026 01:03:17 |
| Eccentricity: | 0.0001470 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 11.4324° |
| argument of perigee: | 77.3561° |
| revolutions per day: | 15.08841338 |
| mean anomaly at epoch: | 282.7596° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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