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 25140.93811318 -.00000035 00000-0 -77203-6 0 9999
2 24278 98.5781 37.4129 0350616 33.6424 328.6449 13.53247611420366
| Epoch (UTC): | 20 May 2025 22:30:52 |
| Eccentricity: | 0.0350616 |
| inclination: | 98.5781° |
| perigee height: | 799 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 37.4129° |
| argument of perigee: | 33.6424° |
| revolutions per day: | 13.53247611 |
| mean anomaly at epoch: | 328.6449° |
| orbit number at epoch: | 42036 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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