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 30596U 99025AMB 24280.71179766 .00004188 00000-0 10901-2 0 9992
2 30596 98.4057 284.1363 0255561 133.9772 288.3087 14.32380391923713
| Epoch (UTC): | 06 October 2024 17:04:59 |
| Eccentricity: | 0.0255561 |
| inclination: | 98.4057° |
| perigee height: | 601 km |
| apogee height: | 967 km |
| right ascension of ascending node: | 284.1363° |
| argument of perigee: | 133.9772° |
| revolutions per day: | 14.32380391 |
| mean anomaly at epoch: | 288.3087° |
| orbit number at epoch: | 92371 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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