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 40042U 14033AJ 24279.83736428 .00036264 00000-0 24224-2 0 9993
2 40042 98.0825 249.0309 0015238 113.9561 246.3262 15.06802790559479
| Epoch (UTC): | 05 October 2024 20:05:48 |
| Eccentricity: | 0.0015238 |
| inclination: | 98.0825° |
| perigee height: | 535 km |
| apogee height: | 556 km |
| right ascension of ascending node: | 249.0309° |
| argument of perigee: | 113.9561° |
| revolutions per day: | 15.06802790 |
| mean anomaly at epoch: | 246.3262° |
| orbit number at epoch: | 55947 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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