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 27130U 01049CA 24276.36234638 .00007905 00000-0 99660-3 0 9997
2 27130 98.2170 306.6647 0014137 318.9238 52.5780 14.82181659226028
| Epoch (UTC): | 02 October 2024 08:41:46 |
| Eccentricity: | 0.0014137 |
| inclination: | 98.2170° |
| perigee height: | 612 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 306.6647° |
| argument of perigee: | 318.9238° |
| revolutions per day: | 14.82181659 |
| mean anomaly at epoch: | 52.5780° |
| orbit number at epoch: | 22602 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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