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 data is extracted from the following two-line orbital elements,
1 00053U 60009E 25348.29332324 .00000041 00000-0 12273-2 0 9995
2 00053 47.2742 192.6773 0097268 249.3982 109.6352 12.17395891912903
| Epoch (UTC): | 14 December 2025 07:02:23 |
| Eccentricity: | 0.0097268 |
| inclination: | 47.2742° |
| perigee height: | 1526 km |
| apogee height: | 1681 km |
| right ascension of ascending node: | 192.6773° |
| argument of perigee: | 249.3982° |
| revolutions per day: | 12.17395891 |
| mean anomaly at epoch: | 109.6352° |
| orbit number at epoch: | 91290 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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