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 25187.81256730 -.00000117 00000-0 -31520-3 0 9993
2 00053 47.2797 327.7010 0100539 135.2726 225.6224 12.17385948893359
| Epoch (UTC): | 06 July 2025 19:30:05 |
| Eccentricity: | 0.0100539 |
| inclination: | 47.2797° |
| perigee height: | 1523 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 327.7010° |
| argument of perigee: | 135.2726° |
| revolutions per day: | 12.17385948 |
| mean anomaly at epoch: | 225.6224° |
| orbit number at epoch: | 89335 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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