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 04793U 26088.11482149 +.00000000 +00000-0 +76324-4 0 00006
2 04793 101.3471 126.3225 0032012 143.0609 283.8301 12.54049530 02
| Epoch (UTC): | 29 March 2026 02:45:20 |
| Eccentricity: | 0.0032012 |
| inclination: | 101.3471° |
| perigee height: | 1423 km |
| apogee height: | 1473 km |
| right ascension of ascending node: | 126.3225° |
| argument of perigee: | 143.0609° |
| revolutions per day: | 12.54049530 |
| mean anomaly at epoch: | 283.8301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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