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 25173.61144483 .00000021 00000-0 10504-2 0 9997
2 00053 47.2792 11.5049 0100380 92.8593 268.3689 12.17385622891624
| Epoch (UTC): | 22 June 2025 14:40:28 |
| Eccentricity: | 0.0100380 |
| inclination: | 47.2792° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 11.5049° |
| argument of perigee: | 92.8593° |
| revolutions per day: | 12.17385622 |
| mean anomaly at epoch: | 268.3689° |
| orbit number at epoch: | 89162 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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