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 is defined by the following mean orbital elements,
1 04047U 26100.03011799 +.00000000 +00000-0 +52963-4 0 00006
2 04047 98.4330 317.6001 0045131 95.5015 265.1317 14.29498826 09
| Epoch (UTC): | 10 April 2026 00:43:22 |
| Eccentricity: | 0.0045131 |
| inclination: | 98.4330° |
| perigee height: | 761 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 317.6001° |
| argument of perigee: | 95.5015° |
| revolutions per day: | 14.29498826 |
| mean anomaly at epoch: | 265.1317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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