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 37388U 26032.49610110 +.00000000 +00000-0 +12641-3 0 00004
2 37388 98.3531 12.7838 0015040 24.7450 85.5937 14.25557949 09
| Epoch (UTC): | 01 February 2026 11:54:23 |
| Eccentricity: | 0.0015040 |
| inclination: | 98.3531° |
| perigee height: | 796 km |
| apogee height: | 817 km |
| right ascension of ascending node: | 12.7838° |
| argument of perigee: | 24.7450° |
| revolutions per day: | 14.25557949 |
| mean anomaly at epoch: | 85.5937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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