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 54185U 26145.60972429 +.00000000 +00000-0 -28634-4 0 00001
2 54185 53.2130 18.5474 0001439 83.8377 276.2779 15.08829759 05
| Epoch (UTC): | 25 May 2026 14:38:00 |
| Eccentricity: | 0.0001439 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 18.5474° |
| argument of perigee: | 83.8377° |
| revolutions per day: | 15.08829759 |
| mean anomaly at epoch: | 276.2779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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