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 24827U 97028A 24278.90686873 -.00000015 00000-0 34364-3 0 9999
2 24827 63.3108 166.3293 1076394 61.5139 12.5129 11.07978273105833
| Epoch (UTC): | 04 October 2024 21:45:53 |
| Eccentricity: | 0.1076394 |
| inclination: | 63.3108° |
| perigee height: | 1206 km |
| apogee height: | 3036 km |
| right ascension of ascending node: | 166.3293° |
| argument of perigee: | 61.5139° |
| revolutions per day: | 11.07978273 |
| mean anomaly at epoch: | 12.5129° |
| orbit number at epoch: | 10583 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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