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 58370U 26145.40769844 +.00000000 +00000-0 +11259-3 0 00007
2 58370 43.0033 277.0590 0001367 269.9390 90.1305 15.27584711 02
| Epoch (UTC): | 25 May 2026 09:47:05 |
| Eccentricity: | 0.0001367 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 277.0590° |
| argument of perigee: | 269.9390° |
| revolutions per day: | 15.27584711 |
| mean anomaly at epoch: | 90.1305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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