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 26037.42801247 +.00000000 +00000-0 +72916-3 0 00004
2 37845 49.6914 78.7108 4512969 121.7657 290.1644 6.44775049 00
| Epoch (UTC): | 06 February 2026 10:16:20 |
| Eccentricity: | 0.4512969 |
| inclination: | 49.6914° |
| perigee height: | 312 km |
| apogee height: | 11318 km |
| right ascension of ascending node: | 78.7108° |
| argument of perigee: | 121.7657° |
| revolutions per day: | 6.44775049 |
| mean anomaly at epoch: | 290.1644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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