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 24278U 96046B 24279.73021464 .00000150 00000-0 19136-3 0 9998
2 24278 98.5809 199.8945 0348943 261.9328 94.2092 13.53214809389384
| Epoch (UTC): | 05 October 2024 17:31:30 |
| Eccentricity: | 0.0348943 |
| inclination: | 98.5809° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 199.8945° |
| argument of perigee: | 261.9328° |
| revolutions per day: | 13.53214809 |
| mean anomaly at epoch: | 94.2092° |
| orbit number at epoch: | 38938 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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