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 26181U 99057BT 23333.43252604 .00002118 00000-0 43613-3 0 9990
2 26181 98.6790 127.9649 0015511 103.7771 315.2813 14.61574109261433
| Epoch (UTC): | 29 November 2023 10:22:50 |
| Eccentricity: | 0.0015511 |
| inclination: | 98.6790° |
| perigee height: | 677 km |
| apogee height: | 699 km |
| right ascension of ascending node: | 127.9649° |
| argument of perigee: | 103.7771° |
| revolutions per day: | 14.61574109 |
| mean anomaly at epoch: | 315.2813° |
| orbit number at epoch: | 26143 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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