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 26931U 01043C 23336.78214457 .00000565 00000-0 24544-3 0 9992
2 26931 67.0500 121.4573 0005738 258.6026 101.4431 14.31058987157706
| Epoch (UTC): | 02 December 2023 18:46:17 |
| Eccentricity: | 0.0005738 |
| inclination: | 67.0500° |
| perigee height: | 784 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 121.4573° |
| argument of perigee: | 258.6026° |
| revolutions per day: | 14.31058987 |
| mean anomaly at epoch: | 101.4431° |
| orbit number at epoch: | 15770 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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