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 39446U 26101.29577487 +.00000000 +00000-0 +32128-3 0 00007
2 39446 97.8649 56.9731 0049361 180.3259 179.7939 14.96515988 04
| Epoch (UTC): | 11 April 2026 07:05:54 |
| Eccentricity: | 0.0049361 |
| inclination: | 97.8649° |
| perigee height: | 543 km |
| apogee height: | 612 km |
| right ascension of ascending node: | 56.9731° |
| argument of perigee: | 180.3259° |
| revolutions per day: | 14.96515988 |
| mean anomaly at epoch: | 179.7939° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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