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 39444U 26066.38481859 +.00000000 +00000-0 +86966-3 0 00001
2 39444 97.8193 35.8839 0037024 187.1122 172.9585 15.07859994 01
| Epoch (UTC): | 07 March 2026 09:14:08 |
| Eccentricity: | 0.0037024 |
| inclination: | 97.8193° |
| perigee height: | 517 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 35.8839° |
| argument of perigee: | 187.1122° |
| revolutions per day: | 15.07859994 |
| mean anomaly at epoch: | 172.9585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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