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 25340.94664658 .00001312 00000-0 20659-3 0 9993
2 00029 48.3774 218.0357 0022261 161.7074 198.4645 14.78401448513682
| Epoch (UTC): | 06 December 2025 22:43:10 |
| Eccentricity: | 0.0022261 |
| inclination: | 48.3774° |
| perigee height: | 619 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 218.0357° |
| argument of perigee: | 161.7074° |
| revolutions per day: | 14.78401448 |
| mean anomaly at epoch: | 198.4645° |
| orbit number at epoch: | 51368 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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