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 53554U 26145.10102391 +.00000000 +00000-0 +25426-4 0 00003
2 53554 53.2143 81.1053 0001574 66.6736 293.4421 15.08840233 00
| Epoch (UTC): | 25 May 2026 02:25:28 |
| Eccentricity: | 0.0001574 |
| inclination: | 53.2143° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 81.1053° |
| argument of perigee: | 66.6736° |
| revolutions per day: | 15.08840233 |
| mean anomaly at epoch: | 293.4421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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