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 25138.79884976 .00000848 00000-0 20891-3 0 9994
2 00047 66.6665 26.0930 0213281 66.7673 295.5733 14.44687229393826
| Epoch (UTC): | 18 May 2025 19:10:20 |
| Eccentricity: | 0.0213281 |
| inclination: | 66.6665° |
| perigee height: | 591 km |
| apogee height: | 895 km |
| right ascension of ascending node: | 26.0930° |
| argument of perigee: | 66.7673° |
| revolutions per day: | 14.44687229 |
| mean anomaly at epoch: | 295.5733° |
| orbit number at epoch: | 39382 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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