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 29U 60002B 25083.25603818 .00002805 00000-0 41422-3 0 9991
2 29 48.3793 1.3881 0022156 131.8633 228.4176 14.77783957475676
| Epoch (UTC): | 24 March 2025 06:08:41 |
| Eccentricity: | 0.0022156 |
| inclination: | 48.3793° |
| perigee height: | 621 km |
| apogee height: | 652 km |
| right ascension of ascending node: | 1.3881° |
| argument of perigee: | 131.8633° |
| revolutions per day: | 14.77783957 |
| mean anomaly at epoch: | 228.4176° |
| orbit number at epoch: | 47567 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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