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 25137.85970774 -.00000084 00000-0 17544-4 0 9994
2 00051 47.2108 192.6302 0106452 102.1498 259.1238 12.18358563882972
| Epoch (UTC): | 17 May 2025 20:37:58 |
| Eccentricity: | 0.0106452 |
| inclination: | 47.2108° |
| perigee height: | 1515 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 192.6302° |
| argument of perigee: | 102.1498° |
| revolutions per day: | 12.18358563 |
| mean anomaly at epoch: | 259.1238° |
| orbit number at epoch: | 88297 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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