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 41064U 00055X 25317.26199533 .00023256 00000-0 70457-2 0 9994
2 41064 98.8458 81.2194 0014299 155.3139 204.8737 14.42172546516825
| Epoch (UTC): | 13 November 2025 06:17:16 |
| Eccentricity: | 0.0014299 |
| inclination: | 98.8458° |
| perigee height: | 741 km |
| apogee height: | 761 km |
| right ascension of ascending node: | 81.2194° |
| argument of perigee: | 155.3139° |
| revolutions per day: | 14.42172546 |
| mean anomaly at epoch: | 204.8737° |
| orbit number at epoch: | 51682 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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