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 37222U 10062A 26008.20159688 0.00001200 00000-0 15112-3 0 09
2 37222 71.9760 158.5408 0015125 61.1373 298.8627 14.81892441 08
| Epoch (UTC): | 08 January 2026 04:50:17 |
| Eccentricity: | 0.0015125 |
| inclination: | 71.9760° |
| perigee height: | 613 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 158.5408° |
| argument of perigee: | 61.1373° |
| revolutions per day: | 14.81892441 |
| mean anomaly at epoch: | 298.8627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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