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 39161U 13021C 25348.89079541 .00001808 00000-0 24183-3 0 9990
2 39161 97.7581 44.3712 0006987 253.9602 106.0841 14.80654300677749
| Epoch (UTC): | 14 December 2025 21:22:44 |
| Eccentricity: | 0.0006987 |
| inclination: | 97.7581° |
| perigee height: | 622 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 44.3712° |
| argument of perigee: | 253.9602° |
| revolutions per day: | 14.80654300 |
| mean anomaly at epoch: | 106.0841° |
| orbit number at epoch: | 67774 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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