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 37162U 10046A 26010.72220873 0.00000000 00000-0 00000-0 0 03
2 37162 122.9973 167.6850 0007274 192.4169 167.5831 13.41447646 00
| Epoch (UTC): | 10 January 2026 17:19:58 |
| Eccentricity: | 0.0007274 |
| inclination: | 122.9973° |
| perigee height: | 1098 km |
| apogee height: | 1109 km |
| right ascension of ascending node: | 167.6850° |
| argument of perigee: | 192.4169° |
| revolutions per day: | 13.41447646 |
| mean anomaly at epoch: | 167.5831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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