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 26071.83035847 +.00000000 +00000-0 +54259-3 0 00002
2 37845 49.7093 42.4552 4512290 152.2981 241.6777 6.45066202 09
| Epoch (UTC): | 12 March 2026 19:55:42 |
| Eccentricity: | 0.4512290 |
| inclination: | 49.7093° |
| perigee height: | 311 km |
| apogee height: | 11312 km |
| right ascension of ascending node: | 42.4552° |
| argument of perigee: | 152.2981° |
| revolutions per day: | 6.45066202 |
| mean anomaly at epoch: | 241.6777° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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