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 57910U 26145.52692743 +.00000000 +00000-0 +20555-3 0 00001
2 57910 43.0022 237.1934 0001612 271.2727 88.7940 15.27583338 03
| Epoch (UTC): | 25 May 2026 12:38:46 |
| Eccentricity: | 0.0001612 |
| inclination: | 43.0022° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 237.1934° |
| argument of perigee: | 271.2727° |
| revolutions per day: | 15.27583338 |
| mean anomaly at epoch: | 88.7940° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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