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 30954U 99025BAU 24280.77493406 .00006649 00000-0 33844-2 0 9991
2 30954 98.7023 26.1192 0132315 339.6041 172.9178 14.11683828902844
| Epoch (UTC): | 06 October 2024 18:35:54 |
| Eccentricity: | 0.0132315 |
| inclination: | 98.7023° |
| perigee height: | 758 km |
| apogee height: | 949 km |
| right ascension of ascending node: | 26.1192° |
| argument of perigee: | 339.6041° |
| revolutions per day: | 14.11683828 |
| mean anomaly at epoch: | 172.9178° |
| orbit number at epoch: | 90284 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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