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 37793U 26104.20691962 +.00000000 +00000-0 +68945-4 0 00006
2 37793 98.2395 13.3935 0041903 291.4699 223.0729 14.76829536 04
| Epoch (UTC): | 14 April 2026 04:57:57 |
| Eccentricity: | 0.0041903 |
| inclination: | 98.2395° |
| perigee height: | 610 km |
| apogee height: | 669 km |
| right ascension of ascending node: | 13.3935° |
| argument of perigee: | 291.4699° |
| revolutions per day: | 14.76829536 |
| mean anomaly at epoch: | 223.0729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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