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 37845U 26072.91468941 +.00000000 +00000-0 +82158-3 0 00006
2 37845 49.7100 41.3122 4512298 153.2589 239.7739 6.45077129 08
| Epoch (UTC): | 13 March 2026 21:57:09 |
| Eccentricity: | 0.4512298 |
| inclination: | 49.7100° |
| perigee height: | 311 km |
| apogee height: | 11312 km |
| right ascension of ascending node: | 41.3122° |
| argument of perigee: | 153.2589° |
| revolutions per day: | 6.45077129 |
| mean anomaly at epoch: | 239.7739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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