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 40069U 14037A 24259.93291708 .00000648 00000-0 31744-3 0 9995
2 40069 98.4446 250.1489 0007038 93.9082 266.2900 14.21060397528513
| Epoch (UTC): | 15 September 2024 22:23:24 |
| Eccentricity: | 0.0007038 |
| inclination: | 98.4446° |
| perigee height: | 817 km |
| apogee height: | 827 km |
| right ascension of ascending node: | 250.1489° |
| argument of perigee: | 93.9082° |
| revolutions per day: | 14.21060397 |
| mean anomaly at epoch: | 266.2900° |
| orbit number at epoch: | 52851 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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