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 25163.50659350 .00000521 00000-0 10045-3 0 9990
2 29 48.3798 340.5152 0022045 117.6835 242.6319 14.78015204487543
| Epoch (UTC): | 12 June 2025 12:09:29 |
| Eccentricity: | 0.0022045 |
| inclination: | 48.3798° |
| perigee height: | 620 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 340.5152° |
| argument of perigee: | 117.6835° |
| revolutions per day: | 14.78015204 |
| mean anomaly at epoch: | 242.6319° |
| orbit number at epoch: | 48754 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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