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 53929U 26145.22527330 +.00000000 +00000-0 +24159-4 0 00008
2 53929 53.2121 330.9130 0001266 89.5227 270.5910 15.08835241 02
| Epoch (UTC): | 25 May 2026 05:24:23 |
| Eccentricity: | 0.0001266 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 330.9130° |
| argument of perigee: | 89.5227° |
| revolutions per day: | 15.08835241 |
| mean anomaly at epoch: | 270.5910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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