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 26088.13097880 +.00000000 +00000-0 +62211-4 0 00004
2 04047 98.4349 306.0796 0044840 129.7687 230.7459 14.29494180 07
| Epoch (UTC): | 29 March 2026 03:08:36 |
| Eccentricity: | 0.0044840 |
| inclination: | 98.4349° |
| perigee height: | 761 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 306.0796° |
| argument of perigee: | 129.7687° |
| revolutions per day: | 14.29494180 |
| mean anomaly at epoch: | 230.7459° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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