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 31220U 99025BLA 24281.39756544 .00261668 00000-0 22988-1 0 9992
2 31220 99.0000 333.0986 0021620 308.5159 62.7496 14.94976993921155
| Epoch (UTC): | 07 October 2024 09:32:29 |
| Eccentricity: | 0.0021620 |
| inclination: | 99.0000° |
| perigee height: | 567 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 333.0986° |
| argument of perigee: | 308.5159° |
| revolutions per day: | 14.94976993 |
| mean anomaly at epoch: | 62.7496° |
| orbit number at epoch: | 92115 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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