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 37841U 26108.57677583 +.00000000 +00000-0 +53580-4 0 00006
2 37841 19.9725 60.2744 0011586 267.7683 248.5244 14.11561078 04
| Epoch (UTC): | 18 April 2026 13:50:33 |
| Eccentricity: | 0.0011586 |
| inclination: | 19.9725° |
| perigee height: | 846 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 60.2744° |
| argument of perigee: | 267.7683° |
| revolutions per day: | 14.11561078 |
| mean anomaly at epoch: | 248.5244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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