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 37387U 26032.39147325 +.00000000 +00000-0 +89011-4 0 00001
2 37387 98.7791 100.6944 0004882 244.5040 115.5632 14.21460564 02
| Epoch (UTC): | 01 February 2026 09:23:43 |
| Eccentricity: | 0.0004882 |
| inclination: | 98.7791° |
| perigee height: | 817 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 100.6944° |
| argument of perigee: | 244.5040° |
| revolutions per day: | 14.21460564 |
| mean anomaly at epoch: | 115.5632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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