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 41667U 00055PG 24356.49731954 .00002435 00000-0 10859-2 0 9995
2 41667 98.7670 91.5754 0029488 307.5822 52.2679 14.23485624450843
| Epoch (UTC): | 21 December 2024 11:56:08 |
| Eccentricity: | 0.0029488 |
| inclination: | 98.7670° |
| perigee height: | 792 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 91.5754° |
| argument of perigee: | 307.5822° |
| revolutions per day: | 14.23485624 |
| mean anomaly at epoch: | 52.2679° |
| orbit number at epoch: | 45084 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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