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 37391U 11014B 26010.73672792 0.00000000 00000-0 00000-0 0 05
2 37391 63.4390 323.3903 0347888 356.3622 3.6198 13.41360574 09
| Epoch (UTC): | 10 January 2026 17:40:53 |
| Eccentricity: | 0.0347888 |
| inclination: | 63.4390° |
| perigee height: | 844 km |
| apogee height: | 1364 km |
| right ascension of ascending node: | 323.3903° |
| argument of perigee: | 356.3622° |
| revolutions per day: | 13.41360574 |
| mean anomaly at epoch: | 3.6198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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