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 26100.17766588 +.00000000 +00000-0 +12929-3 0 00003
2 00809 90.4482 174.4646 0037575 281.4349 78.2617 14.10762170 06
| Epoch (UTC): | 10 April 2026 04:15:50 |
| Eccentricity: | 0.0037575 |
| inclination: | 90.4482° |
| perigee height: | 830 km |
| apogee height: | 884 km |
| right ascension of ascending node: | 174.4646° |
| argument of perigee: | 281.4349° |
| revolutions per day: | 14.10762170 |
| mean anomaly at epoch: | 78.2617° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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