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 53205U 26145.13393097 +.00000000 +00000-0 -79409-3 0 00004
2 53205 97.4463 206.2175 0000141 337.7640 22.3581 15.05712884 01
| Epoch (UTC): | 25 May 2026 03:12:51 |
| Eccentricity: | 0.0000141 |
| inclination: | 97.4463° |
| perigee height: | 549 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 206.2175° |
| argument of perigee: | 337.7640° |
| revolutions per day: | 15.05712884 |
| mean anomaly at epoch: | 22.3581° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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