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 26109.24233679 +.00000000 +00000-0 +46927-3 0 00002
2 39444 97.8250 79.5096 0038470 46.7073 313.7353 15.08634976 06
| Epoch (UTC): | 19 April 2026 05:48:57 |
| Eccentricity: | 0.0038470 |
| inclination: | 97.8250° |
| perigee height: | 514 km |
| apogee height: | 567 km |
| right ascension of ascending node: | 79.5096° |
| argument of perigee: | 46.7073° |
| revolutions per day: | 15.08634976 |
| mean anomaly at epoch: | 313.7353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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