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 00047U 60007C 25173.34336074 .00000182 00000-0 63774-4 0 9994
2 00047 66.6656 293.3429 0215111 40.6732 321.0215 14.44731023398815
| Epoch (UTC): | 22 June 2025 08:14:26 |
| Eccentricity: | 0.0215111 |
| inclination: | 66.6656° |
| perigee height: | 590 km |
| apogee height: | 896 km |
| right ascension of ascending node: | 293.3429° |
| argument of perigee: | 40.6732° |
| revolutions per day: | 14.44731023 |
| mean anomaly at epoch: | 321.0215° |
| orbit number at epoch: | 39881 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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