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 26139.96329214 +.00000000 +00000-0 +50483-4 0 00007
2 37841 19.9713 230.3070 0011590 253.8577 262.4543 14.11568954 03
| Epoch (UTC): | 19 May 2026 23:07:08 |
| Eccentricity: | 0.0011590 |
| inclination: | 19.9713° |
| perigee height: | 846 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 230.3070° |
| argument of perigee: | 253.8577° |
| revolutions per day: | 14.11568954 |
| mean anomaly at epoch: | 262.4543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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