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 58128U 26145.12009084 +.00000000 +00000-0 +12406-4 0 00006
2 58128 43.0046 57.6539 0000891 259.0772 100.9979 15.27573971 00
| Epoch (UTC): | 25 May 2026 02:52:55 |
| Eccentricity: | 0.0000891 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 57.6539° |
| argument of perigee: | 259.0772° |
| revolutions per day: | 15.27573971 |
| mean anomaly at epoch: | 100.9979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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