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 25338.68918556 -.00000089 00000-0 -47348-4 0 9991
2 00053 47.2757 222.3027 0097381 221.2477 138.0923 12.17394718911733
| Epoch (UTC): | 04 December 2025 16:32:25 |
| Eccentricity: | 0.0097381 |
| inclination: | 47.2757° |
| perigee height: | 1526 km |
| apogee height: | 1681 km |
| right ascension of ascending node: | 222.3027° |
| argument of perigee: | 221.2477° |
| revolutions per day: | 12.17394718 |
| mean anomaly at epoch: | 138.0923° |
| orbit number at epoch: | 91173 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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