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 37220U 26070.48093988 +.00000000 +00000-0 +52289-3 0 00000
2 37220 49.4200 75.0085 5392197 53.7067 344.9936 4.91345195 03
| Epoch (UTC): | 11 March 2026 11:32:33 |
| Eccentricity: | 0.5392197 |
| inclination: | 49.4200° |
| perigee height: | 356 km |
| apogee height: | 16118 km |
| right ascension of ascending node: | 75.0085° |
| argument of perigee: | 53.7067° |
| revolutions per day: | 4.91345195 |
| mean anomaly at epoch: | 344.9936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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