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 25171.31298266 -.00000003 00000-0 81115-3 0 9999
2 00053 47.2791 18.5949 0100358 85.9896 275.2358 12.17385289891341
| Epoch (UTC): | 20 June 2025 07:30:41 |
| Eccentricity: | 0.0100358 |
| inclination: | 47.2791° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 18.5949° |
| argument of perigee: | 85.9896° |
| revolutions per day: | 12.17385289 |
| mean anomaly at epoch: | 275.2358° |
| orbit number at epoch: | 89134 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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