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 31402U 88005X 24355.77151773 .00004614 00000-0 30128-2 0 9999
2 31402 82.5422 348.6137 0010948 356.1280 178.1738 14.02051438922460
| Epoch (UTC): | 20 December 2024 18:30:59 |
| Eccentricity: | 0.0010948 |
| inclination: | 82.5422° |
| perigee height: | 879 km |
| apogee height: | 894 km |
| right ascension of ascending node: | 348.6137° |
| argument of perigee: | 356.1280° |
| revolutions per day: | 14.02051438 |
| mean anomaly at epoch: | 178.1738° |
| orbit number at epoch: | 92246 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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