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 26071.09143830 +.00000000 +00000-0 +46455-3 0 00008
2 37220 49.4201 74.5762 5392251 54.0777 344.8678 4.91346195 06
| Epoch (UTC): | 12 March 2026 02:11:40 |
| Eccentricity: | 0.5392251 |
| inclination: | 49.4201° |
| perigee height: | 356 km |
| apogee height: | 16118 km |
| right ascension of ascending node: | 74.5762° |
| argument of perigee: | 54.0777° |
| revolutions per day: | 4.91346195 |
| mean anomaly at epoch: | 344.8678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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