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 25137.69118857 .00000915 00000-0 22356-3 0 9993
2 00047 66.6666 29.0667 0213247 67.6112 294.7435 14.44685522393663
| Epoch (UTC): | 17 May 2025 16:35:18 |
| Eccentricity: | 0.0213247 |
| inclination: | 66.6666° |
| perigee height: | 591 km |
| apogee height: | 895 km |
| right ascension of ascending node: | 29.0667° |
| argument of perigee: | 67.6112° |
| revolutions per day: | 14.44685522 |
| mean anomaly at epoch: | 294.7435° |
| orbit number at epoch: | 39366 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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