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 25166.71604581 -.00000110 00000-0 -23246-3 0 9999
2 00053 47.2790 32.7745 0100342 72.3005 288.8708 12.17384692890780
| Epoch (UTC): | 15 June 2025 17:11:06 |
| Eccentricity: | 0.0100342 |
| inclination: | 47.2790° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 32.7745° |
| argument of perigee: | 72.3005° |
| revolutions per day: | 12.17384692 |
| mean anomaly at epoch: | 288.8708° |
| orbit number at epoch: | 89078 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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