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 25967U 99063A 23271.16299493 -.00000194 00000-0 00000+0 0 9998
2 25967 9.2991 31.7153 0005188 162.8673 208.2573 1.00272811 87381
| Epoch (UTC): | 28 September 2023 03:54:42 |
| Eccentricity: | 0.0005188 |
| inclination: | 9.2991° |
| perigee height: | 35764 km |
| apogee height: | 35808 km |
| right ascension of ascending node: | 31.7153° |
| argument of perigee: | 162.8673° |
| revolutions per day: | 1.00272811 |
| mean anomaly at epoch: | 208.2573° |
| orbit number at epoch: | 8738 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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