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 25173.45681462 -.00000031 00000-0 51853-3 0 9995
2 00051 47.2134 82.4815 0106493 207.5946 151.9163 12.18362013887313
| Epoch (UTC): | 22 June 2025 10:57:48 |
| Eccentricity: | 0.0106493 |
| inclination: | 47.2134° |
| perigee height: | 1515 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 82.4815° |
| argument of perigee: | 207.5946° |
| revolutions per day: | 12.18362013 |
| mean anomaly at epoch: | 151.9163° |
| orbit number at epoch: | 88731 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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