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 57324U 23091AY 24279.88721843 .00077163 00000-0 33221-2 0 9998
2 57324 97.5968 333.8417 0014182 97.7553 262.5293 15.22201121 68255
| Epoch (UTC): | 05 October 2024 21:17:35 |
| Eccentricity: | 0.0014182 |
| inclination: | 97.5968° |
| perigee height: | 489 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 333.8417° |
| argument of perigee: | 97.7553° |
| revolutions per day: | 15.22201121 |
| mean anomaly at epoch: | 262.5293° |
| orbit number at epoch: | 6825 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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