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 60235U 24128A 25200.81855156 .00001657 00000-0 14846-3 0 9996
2 60235 61.9952 305.4750 0060104 59.7520 300.9500 14.98897203 56147
| Epoch (UTC): | 19 July 2025 19:38:42 |
| Eccentricity: | 0.0060104 |
| inclination: | 61.9952° |
| perigee height: | 528 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 305.4750° |
| argument of perigee: | 59.7520° |
| revolutions per day: | 14.98897203 |
| mean anomaly at epoch: | 300.9500° |
| orbit number at epoch: | 5614 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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