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 00809U 26088.19076432 +.00000000 +00000-0 +14682-3 0 00000
2 00809 90.4495 173.8619 0038275 321.8948 37.9531 14.10753964 03
| Epoch (UTC): | 29 March 2026 04:34:42 |
| Eccentricity: | 0.0038275 |
| inclination: | 90.4495° |
| perigee height: | 829 km |
| apogee height: | 884 km |
| right ascension of ascending node: | 173.8619° |
| argument of perigee: | 321.8948° |
| revolutions per day: | 14.10753964 |
| mean anomaly at epoch: | 37.9531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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