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 25073.58168861 .00001967 00000-0 45333-3 0 9998
2 00047 66.6660 201.1615 0213894 116.3533 245.9709 14.44507141384404
| Epoch (UTC): | 14 March 2025 13:57:37 |
| Eccentricity: | 0.0213894 |
| inclination: | 66.6660° |
| perigee height: | 591 km |
| apogee height: | 896 km |
| right ascension of ascending node: | 201.1615° |
| argument of perigee: | 116.3533° |
| revolutions per day: | 14.44507141 |
| mean anomaly at epoch: | 245.9709° |
| orbit number at epoch: | 38440 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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