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 41857U 16068A 24358.45874739 .00000688 00000-0 26656-3 0 9995
2 41857 98.5923 3.0923 0006485 150.5201 209.6350 14.33148513424397
| Epoch (UTC): | 23 December 2024 11:00:35 |
| Eccentricity: | 0.0006485 |
| inclination: | 98.5923° |
| perigee height: | 776 km |
| apogee height: | 786 km |
| right ascension of ascending node: | 3.0923° |
| argument of perigee: | 150.5201° |
| revolutions per day: | 14.33148513 |
| mean anomaly at epoch: | 209.6350° |
| orbit number at epoch: | 42439 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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