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 29499U 06044A 25133.97308683 .00001494 00000-0 18486-3 0 9993
2 29499 98.3297 223.9886 0178274 260.3305 263.8897 14.73897066966600
| Epoch (UTC): | 13 May 2025 23:21:14 |
| Eccentricity: | 0.0178274 |
| inclination: | 98.3297° |
| perigee height: | 523 km |
| apogee height: | 774 km |
| right ascension of ascending node: | 223.9886° |
| argument of perigee: | 260.3305° |
| revolutions per day: | 14.73897066 |
| mean anomaly at epoch: | 263.8897° |
| orbit number at epoch: | 96660 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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