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 30349U 99025ABL 24279.87196300 .00012911 00000-0 75790-2 0 9996
2 30349 98.5525 257.3815 0092828 160.4409 262.9523 14.06057203901354
| Epoch (UTC): | 05 October 2024 20:55:37 |
| Eccentricity: | 0.0092828 |
| inclination: | 98.5525° |
| perigee height: | 805 km |
| apogee height: | 940 km |
| right ascension of ascending node: | 257.3815° |
| argument of perigee: | 160.4409° |
| revolutions per day: | 14.06057203 |
| mean anomaly at epoch: | 262.9523° |
| orbit number at epoch: | 90135 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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