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 40907U 15049J 23335.12486250 .00030181 00000-0 87962-3 0 9991
2 40907 97.4877 344.5265 0006897 290.0543 69.9957 15.35306300454033
| Epoch (UTC): | 01 December 2023 02:59:48 |
| Eccentricity: | 0.0006897 |
| inclination: | 97.4877° |
| perigee height: | 455 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 344.5265° |
| argument of perigee: | 290.0543° |
| revolutions per day: | 15.35306300 |
| mean anomaly at epoch: | 69.9957° |
| orbit number at epoch: | 45403 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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