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 23628U 95038A 23267.78493328 -.00000091 00000-0 00000-0 0 9991
2 23628 12.4894 22.1028 0004687 142.7885 224.8077 0.98663413 22932
| Epoch (UTC): | 24 September 2023 18:50:18 |
| Eccentricity: | 0.0004687 |
| inclination: | 12.4894° |
| perigee height: | 36223 km |
| apogee height: | 36263 km |
| right ascension of ascending node: | 22.1028° |
| argument of perigee: | 142.7885° |
| revolutions per day: | 0.98663413 |
| mean anomaly at epoch: | 224.8077° |
| orbit number at epoch: | 2293 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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