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 40471U 95015BP 25316.78973133 .00009757 00000-0 39927-2 0 9994
2 40471 98.9006 337.4184 0020853 223.7694 136.1833 14.27282498551330
| Epoch (UTC): | 12 November 2025 18:57:12 |
| Eccentricity: | 0.0020853 |
| inclination: | 98.9006° |
| perigee height: | 786 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 337.4184° |
| argument of perigee: | 223.7694° |
| revolutions per day: | 14.27282498 |
| mean anomaly at epoch: | 136.1833° |
| orbit number at epoch: | 55133 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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