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 30619U 99025ANA 24281.03854783 .00005666 00000-0 13933-2 0 9993
2 30619 98.3401 309.7854 0219296 279.5924 78.0550 14.39136534927359
| Epoch (UTC): | 07 October 2024 00:55:30 |
| Eccentricity: | 0.0219296 |
| inclination: | 98.3401° |
| perigee height: | 605 km |
| apogee height: | 918 km |
| right ascension of ascending node: | 309.7854° |
| argument of perigee: | 279.5924° |
| revolutions per day: | 14.39136534 |
| mean anomaly at epoch: | 78.0550° |
| orbit number at epoch: | 92735 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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