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 23967U 96042A 23088.54122426 .00000102 00000-0 00000-0 0 9998
2 23967 10.0338 22.5124 0008678 66.4880 130.4465 1.00215760 97697
| Epoch (UTC): | 29 March 2023 12:59:21 |
| Eccentricity: | 0.0008678 |
| inclination: | 10.0338° |
| perigee height: | 35765 km |
| apogee height: | 35838 km |
| right ascension of ascending node: | 22.5124° |
| argument of perigee: | 66.4880° |
| revolutions per day: | 1.00215760 |
| mean anomaly at epoch: | 130.4465° |
| orbit number at epoch: | 9769 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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