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 58750U 26145.46898110 +.00000000 +00000-0 +53892-4 0 00004
2 58750 43.0037 146.3528 0001794 274.6954 85.3693 15.27579376 07
| Epoch (UTC): | 25 May 2026 11:15:19 |
| Eccentricity: | 0.0001794 |
| inclination: | 43.0037° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 146.3528° |
| argument of perigee: | 274.6954° |
| revolutions per day: | 15.27579376 |
| mean anomaly at epoch: | 85.3693° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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