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 39150U 26118.86390727 +.00000000 +00000-0 +69511-4 0 00007
2 39150 97.9114 191.9289 0018411 66.9803 293.3347 14.76518985 02
| Epoch (UTC): | 28 April 2026 20:44:01 |
| Eccentricity: | 0.0018411 |
| inclination: | 97.9114° |
| perigee height: | 627 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 191.9289° |
| argument of perigee: | 66.9803° |
| revolutions per day: | 14.76518985 |
| mean anomaly at epoch: | 293.3347° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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