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 43071U 26145.22309421 +.00000000 +00000-0 +16551-4 0 00001
2 43071 86.3970 331.3123 0002440 91.7428 268.4047 14.34217708 05
| Epoch (UTC): | 25 May 2026 05:21:15 |
| Eccentricity: | 0.0002440 |
| inclination: | 86.3970° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 331.3123° |
| argument of perigee: | 91.7428° |
| revolutions per day: | 14.34217708 |
| mean anomaly at epoch: | 268.4047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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