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 53824U 26145.48639706 +.00000000 +00000-0 +14527-4 0 00009
2 53824 53.2147 318.7726 0001385 84.9962 275.1189 15.08837668 00
| Epoch (UTC): | 25 May 2026 11:40:24 |
| Eccentricity: | 0.0001385 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 318.7726° |
| argument of perigee: | 84.9962° |
| revolutions per day: | 15.08837668 |
| mean anomaly at epoch: | 275.1189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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