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 26022.24276536 +.00000000 +00000-0 +11380-2 0 00009
2 37220 49.3929 109.1772 5392293 24.3643 353.7514 4.91182122 02
| Epoch (UTC): | 22 January 2026 05:49:34 |
| Eccentricity: | 0.5392293 |
| inclination: | 49.3929° |
| perigee height: | 358 km |
| apogee height: | 16123 km |
| right ascension of ascending node: | 109.1772° |
| argument of perigee: | 24.3643° |
| revolutions per day: | 4.91182122 |
| mean anomaly at epoch: | 353.7514° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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