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 57883U 26145.46457132 +.00000000 +00000-0 +26094-4 0 00009
2 57883 43.0029 211.2350 0001590 269.9225 90.1445 15.27579518 08
| Epoch (UTC): | 25 May 2026 11:08:58 |
| Eccentricity: | 0.0001590 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.2350° |
| argument of perigee: | 269.9225° |
| revolutions per day: | 15.27579518 |
| mean anomaly at epoch: | 90.1445° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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