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 24262.35506164 .00000058 00000-0 98499-4 0 9990
2 24278 98.5798 184.7934 0349205 307.0774 49.8909 13.53210784387032
| Epoch (UTC): | 18 September 2024 08:31:17 |
| Eccentricity: | 0.0349205 |
| inclination: | 98.5798° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 184.7934° |
| argument of perigee: | 307.0774° |
| revolutions per day: | 13.53210784 |
| mean anomaly at epoch: | 49.8909° |
| orbit number at epoch: | 38703 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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