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 23467U 95003A 23272.55655271 -.00000030 00000-0 00000-0 0 9995
2 23467 9.7871 16.2660 0005294 156.4077 208.1272 1.00275341105019
| Epoch (UTC): | 29 September 2023 13:21:26 |
| Eccentricity: | 0.0005294 |
| inclination: | 9.7871° |
| perigee height: | 35763 km |
| apogee height: | 35807 km |
| right ascension of ascending node: | 16.2660° |
| argument of perigee: | 156.4077° |
| revolutions per day: | 1.00275341 |
| mean anomaly at epoch: | 208.1272° |
| orbit number at epoch: | 10501 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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