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 43252U 26145.39091876 +.00000000 +00000-0 +68863-4 0 00005
2 43252 86.3939 299.9681 0002171 90.3524 269.7920 14.34219103 07
| Epoch (UTC): | 25 May 2026 09:22:55 |
| Eccentricity: | 0.0002171 |
| inclination: | 86.3939° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 299.9681° |
| argument of perigee: | 90.3524° |
| revolutions per day: | 14.34219103 |
| mean anomaly at epoch: | 269.7920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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