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 59112U 24043Q 25018.85899138 .00022023 00000-0 79399-3 0 9997
2 59112 97.4959 148.1139 0011655 257.6567 102.3368 15.28491212 48635
| Epoch (UTC): | 18 January 2025 20:36:56 |
| Eccentricity: | 0.0011655 |
| inclination: | 97.4959° |
| perigee height: | 472 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 148.1139° |
| argument of perigee: | 257.6567° |
| revolutions per day: | 15.28491212 |
| mean anomaly at epoch: | 102.3368° |
| orbit number at epoch: | 4863 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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