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 39439U 26037.92327700 +.00000000 +00000-0 +27520-2 0 00007
2 39439 97.7434 32.7827 0012268 157.6846 202.4957 15.79361733 03
| Epoch (UTC): | 06 February 2026 22:09:31 |
| Eccentricity: | 0.0012268 |
| inclination: | 97.7434° |
| perigee height: | 324 km |
| apogee height: | 340 km |
| right ascension of ascending node: | 32.7827° |
| argument of perigee: | 157.6846° |
| revolutions per day: | 15.79361733 |
| mean anomaly at epoch: | 202.4957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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