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 25347.94635943 .00002509 00000-0 29842-3 0 9995
2 29499 98.3297 84.0648 0175309 299.9575 199.5997 14.75030912998135
| Epoch (UTC): | 13 December 2025 22:42:45 |
| Eccentricity: | 0.0175309 |
| inclination: | 98.3297° |
| perigee height: | 522 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 84.0648° |
| argument of perigee: | 299.9575° |
| revolutions per day: | 14.75030912 |
| mean anomaly at epoch: | 199.5997° |
| orbit number at epoch: | 99813 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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