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 37241U 26088.07484213 +.00000000 +00000-0 +39838-3 0 00007
2 37241 98.9599 262.6378 0022277 80.1632 280.2062 14.28449762 09
| Epoch (UTC): | 29 March 2026 01:47:46 |
| Eccentricity: | 0.0022277 |
| inclination: | 98.9599° |
| perigee height: | 781 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 262.6378° |
| argument of perigee: | 80.1632° |
| revolutions per day: | 14.28449762 |
| mean anomaly at epoch: | 280.2062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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