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 00029U 60002B 25340.67630336 .00001403 00000-0 21886-3 0 9993
2 00029 48.3773 219.3196 0022249 160.5899 199.5866 14.78401161513649
| Epoch (UTC): | 06 December 2025 16:13:52 |
| Eccentricity: | 0.0022249 |
| inclination: | 48.3773° |
| perigee height: | 619 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 219.3196° |
| argument of perigee: | 160.5899° |
| revolutions per day: | 14.78401161 |
| mean anomaly at epoch: | 199.5866° |
| orbit number at epoch: | 51364 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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