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 26105.85963904 +.00000000 +00000-0 +33985-3 0 00006
2 39444 97.8233 76.0625 0038549 57.5687 302.9260 15.08594905 09
| Epoch (UTC): | 15 April 2026 20:37:52 |
| Eccentricity: | 0.0038549 |
| inclination: | 97.8233° |
| perigee height: | 514 km |
| apogee height: | 567 km |
| right ascension of ascending node: | 76.0625° |
| argument of perigee: | 57.5687° |
| revolutions per day: | 15.08594905 |
| mean anomaly at epoch: | 302.9260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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