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 41400U 00055KD 23337.08712733 .00006509 00000-0 29492-2 0 9996
2 41400 98.7466 57.9329 0020077 89.9864 270.3614 14.22146318400061
| Epoch (UTC): | 03 December 2023 02:05:27 |
| Eccentricity: | 0.0020077 |
| inclination: | 98.7466° |
| perigee height: | 803 km |
| apogee height: | 832 km |
| right ascension of ascending node: | 57.9329° |
| argument of perigee: | 89.9864° |
| revolutions per day: | 14.22146318 |
| mean anomaly at epoch: | 270.3614° |
| orbit number at epoch: | 40006 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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