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 24834U 97029A 23269.85458372 -.00000119 00000-0 00000-0 0 9994
2 24834 15.1569 12.9371 0102114 212.5839 149.2513 0.96050499 93854
| Epoch (UTC): | 26 September 2023 20:30:36 |
| Eccentricity: | 0.0102114 |
| inclination: | 15.1569° |
| perigee height: | 36569 km |
| apogee height: | 37456 km |
| right ascension of ascending node: | 12.9371° |
| argument of perigee: | 212.5839° |
| revolutions per day: | 0.96050499 |
| mean anomaly at epoch: | 149.2513° |
| orbit number at epoch: | 9385 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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