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 18959U 88020B 24284.53794417 .00002078 00000-0 24156-3 0 9998
2 18959 82.5341 292.5742 0015247 324.7567 35.2639 14.84832936976818
| Epoch (UTC): | 10 October 2024 12:54:38 |
| Eccentricity: | 0.0015247 |
| inclination: | 82.5341° |
| perigee height: | 603 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 292.5742° |
| argument of perigee: | 324.7567° |
| revolutions per day: | 14.84832936 |
| mean anomaly at epoch: | 35.2639° |
| orbit number at epoch: | 97681 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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