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 26101.34924762 +.00000000 +00000-0 +40009-3 0 00000
2 39444 97.8224 71.4683 0038861 72.3239 288.2226 15.08545148 00
| Epoch (UTC): | 11 April 2026 08:22:54 |
| Eccentricity: | 0.0038861 |
| inclination: | 97.8224° |
| perigee height: | 514 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 71.4683° |
| argument of perigee: | 72.3239° |
| revolutions per day: | 15.08545148 |
| mean anomaly at epoch: | 288.2226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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