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 40025U 14033R 24260.96216279 .00015749 00000-0 11986-2 0 9991
2 40025 98.0539 224.9189 0010284 215.3346 144.7197 15.02153247557157
| Epoch (UTC): | 16 September 2024 23:05:30 |
| Eccentricity: | 0.0010284 |
| inclination: | 98.0539° |
| perigee height: | 553 km |
| apogee height: | 567 km |
| right ascension of ascending node: | 224.9189° |
| argument of perigee: | 215.3346° |
| revolutions per day: | 15.02153247 |
| mean anomaly at epoch: | 144.7197° |
| orbit number at epoch: | 55715 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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