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 10096U 77055B 24276.41963891 .00003185 00000-0 32103-3 0 9991
2 10096 75.8333 304.1408 0042120 257.0569 102.5917 14.90720391558560
| Epoch (UTC): | 02 October 2024 10:04:16 |
| Eccentricity: | 0.0042120 |
| inclination: | 75.8333° |
| perigee height: | 566 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 304.1408° |
| argument of perigee: | 257.0569° |
| revolutions per day: | 14.90720391 |
| mean anomaly at epoch: | 102.5917° |
| orbit number at epoch: | 55856 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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