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 00012U 59001B 24280.61127525 .00003620 00000-0 21278-2 0 9996
2 00012 32.8973 243.1605 1652841 72.4126 304.9685 11.47222206460223
| Epoch (UTC): | 06 October 2024 14:40:14 |
| Eccentricity: | 0.1652841 |
| inclination: | 32.8973° |
| perigee height: | 553 km |
| apogee height: | 3299 km |
| right ascension of ascending node: | 243.1605° |
| argument of perigee: | 72.4126° |
| revolutions per day: | 11.47222206 |
| mean anomaly at epoch: | 304.9685° |
| orbit number at epoch: | 46022 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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