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 43253U 26145.37823375 +.00000000 +00000-0 +67929-4 0 00003
2 43253 86.3939 299.9457 0001882 87.6685 272.4726 14.34218858 05
| Epoch (UTC): | 25 May 2026 09:04:39 |
| Eccentricity: | 0.0001882 |
| inclination: | 86.3939° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 299.9457° |
| argument of perigee: | 87.6685° |
| revolutions per day: | 14.34218858 |
| mean anomaly at epoch: | 272.4726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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