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 58787U 26145.54107840 +.00000000 +00000-0 +38553-4 0 00003
2 58787 43.0006 90.8697 0000919 260.8049 99.2699 15.27575863 00
| Epoch (UTC): | 25 May 2026 12:59:09 |
| Eccentricity: | 0.0000919 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 90.8697° |
| argument of perigee: | 260.8049° |
| revolutions per day: | 15.27575863 |
| mean anomaly at epoch: | 99.2699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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