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 00051U 60009C 25347.50637919 .00000029 00000-0 11089-2 0 9994
2 00051 47.2129 263.9246 0111289 4.3707 355.8031 12.18377472908530
| Epoch (UTC): | 13 December 2025 12:09:11 |
| Eccentricity: | 0.0111289 |
| inclination: | 47.2129° |
| perigee height: | 1511 km |
| apogee height: | 1688 km |
| right ascension of ascending node: | 263.9246° |
| argument of perigee: | 4.3707° |
| revolutions per day: | 12.18377472 |
| mean anomaly at epoch: | 355.8031° |
| orbit number at epoch: | 90853 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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