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 00652U 61015HD 25339.14893274 .00003727 00000-0 18182-2 0 9997
2 00652 66.7058 244.4299 0068324 140.4091 220.2019 14.17900417266344
| Epoch (UTC): | 05 December 2025 03:34:27 |
| Eccentricity: | 0.0068324 |
| inclination: | 66.7058° |
| perigee height: | 783 km |
| apogee height: | 882 km |
| right ascension of ascending node: | 244.4299° |
| argument of perigee: | 140.4091° |
| revolutions per day: | 14.17900417 |
| mean anomaly at epoch: | 220.2019° |
| orbit number at epoch: | 26634 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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