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 29769U 99025BK 24280.05050047 .00012639 00000-0 68986-2 0 9995
2 29769 99.1394 323.9343 0096128 264.2028 94.8176 14.09840501905750
| Epoch (UTC): | 06 October 2024 01:12:43 |
| Eccentricity: | 0.0096128 |
| inclination: | 99.1394° |
| perigee height: | 790 km |
| apogee height: | 929 km |
| right ascension of ascending node: | 323.9343° |
| argument of perigee: | 264.2028° |
| revolutions per day: | 14.09840501 |
| mean anomaly at epoch: | 94.8176° |
| orbit number at epoch: | 90575 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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