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 30289U 99025ZA 24281.51254191 .00022113 00000-0 10427-1 0 9996
2 30289 98.9336 6.0033 0044774 133.4195 349.7483 14.19269797909591
| Epoch (UTC): | 07 October 2024 12:18:03 |
| Eccentricity: | 0.0044774 |
| inclination: | 98.9336° |
| perigee height: | 795 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 6.0033° |
| argument of perigee: | 133.4195° |
| revolutions per day: | 14.19269797 |
| mean anomaly at epoch: | 349.7483° |
| orbit number at epoch: | 90959 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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