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 42423U 00055TT 24355.80197287 .00052953 00000-0 12391-1 0 9997
2 42423 98.9245 121.9144 0019991 206.7207 153.2959 14.54194677449176
| Epoch (UTC): | 20 December 2024 19:14:50 |
| Eccentricity: | 0.0019991 |
| inclination: | 98.9245° |
| perigee height: | 698 km |
| apogee height: | 726 km |
| right ascension of ascending node: | 121.9144° |
| argument of perigee: | 206.7207° |
| revolutions per day: | 14.54194677 |
| mean anomaly at epoch: | 153.2959° |
| orbit number at epoch: | 44917 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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