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 24340U 94029NR 23335.39922585 .00002273 00000-0 10096-2 0 9998
2 24340 81.5671 325.0542 0871442 242.6341 108.3519 13.06251801403755
| Epoch (UTC): | 01 December 2023 09:34:53 |
| Eccentricity: | 0.0871442 |
| inclination: | 81.5671° |
| perigee height: | 574 km |
| apogee height: | 1901 km |
| right ascension of ascending node: | 325.0542° |
| argument of perigee: | 242.6341° |
| revolutions per day: | 13.06251801 |
| mean anomaly at epoch: | 108.3519° |
| orbit number at epoch: | 40375 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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