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 53546U 26145.21133238 +.00000000 +00000-0 -62851-5 0 00005
2 53546 53.2133 70.1302 0001335 63.4573 296.6556 15.08833351 01
| Epoch (UTC): | 25 May 2026 05:04:19 |
| Eccentricity: | 0.0001335 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 70.1302° |
| argument of perigee: | 63.4573° |
| revolutions per day: | 15.08833351 |
| mean anomaly at epoch: | 296.6556° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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