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 26106.65557581 +.00000000 +00000-0 +36089-3 0 00003
2 39444 97.8238 76.8736 0038542 54.9890 305.4945 15.08603541 00
| Epoch (UTC): | 16 April 2026 15:44:01 |
| Eccentricity: | 0.0038542 |
| inclination: | 97.8238° |
| perigee height: | 514 km |
| apogee height: | 567 km |
| right ascension of ascending node: | 76.8736° |
| argument of perigee: | 54.9890° |
| revolutions per day: | 15.08603541 |
| mean anomaly at epoch: | 305.4945° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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