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 24279.36991114 .00006525 00000-0 16023-2 0 9994
2 30619 98.3400 308.1608 0219381 284.6425 73.0534 14.39121037927119
| Epoch (UTC): | 05 October 2024 08:52:40 |
| Eccentricity: | 0.0219381 |
| inclination: | 98.3400° |
| perigee height: | 605 km |
| apogee height: | 918 km |
| right ascension of ascending node: | 308.1608° |
| argument of perigee: | 284.6425° |
| revolutions per day: | 14.39121037 |
| mean anomaly at epoch: | 73.0534° |
| orbit number at epoch: | 92711 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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