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 53533U 26145.10650502 +.00000000 +00000-0 +31151-4 0 00004
2 53533 53.2150 91.0600 0001285 73.1422 286.9711 15.08843881 08
| Epoch (UTC): | 25 May 2026 02:33:22 |
| Eccentricity: | 0.0001285 |
| inclination: | 53.2150° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 91.0600° |
| argument of perigee: | 73.1422° |
| revolutions per day: | 15.08843881 |
| mean anomaly at epoch: | 286.9711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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