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 53722U 26145.32178227 +.00000000 +00000-0 +81328-5 0 00009
2 53722 53.2134 270.0142 0001438 85.2817 274.8339 15.08836720 08
| Epoch (UTC): | 25 May 2026 07:43:21 |
| Eccentricity: | 0.0001438 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 270.0142° |
| argument of perigee: | 85.2817° |
| revolutions per day: | 15.08836720 |
| mean anomaly at epoch: | 274.8339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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