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 42586U 73086JA 24355.76707556 .00000039 00000-0 67246-3 0 9991
2 42586 102.4062 3.0852 0030880 62.3796 112.3027 12.35421811499761
| Epoch (UTC): | 20 December 2024 18:24:35 |
| Eccentricity: | 0.0030880 |
| inclination: | 102.4062° |
| perigee height: | 1501 km |
| apogee height: | 1550 km |
| right ascension of ascending node: | 3.0852° |
| argument of perigee: | 62.3796° |
| revolutions per day: | 12.35421811 |
| mean anomaly at epoch: | 112.3027° |
| orbit number at epoch: | 49976 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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