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 43678U 18084H 24263.47537191 .00004450 00000-0 40161-3 0 9991
2 43678 98.0838 64.3297 0010324 80.9262 279.3126 14.96018128321011
| Epoch (UTC): | 19 September 2024 11:24:32 |
| Eccentricity: | 0.0010324 |
| inclination: | 98.0838° |
| perigee height: | 572 km |
| apogee height: | 586 km |
| right ascension of ascending node: | 64.3297° |
| argument of perigee: | 80.9262° |
| revolutions per day: | 14.96018128 |
| mean anomaly at epoch: | 279.3126° |
| orbit number at epoch: | 32101 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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