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 01576U 26087.01821927 +.00000000 +00000-0 +23720-2 0 00001
2 01576 34.2296 46.6223 1380234 305.1983 42.6873 11.82564286 03
| Epoch (UTC): | 28 March 2026 00:26:14 |
| Eccentricity: | 0.1380234 |
| inclination: | 34.2296° |
| perigee height: | 637 km |
| apogee height: | 2883 km |
| right ascension of ascending node: | 46.6223° |
| argument of perigee: | 305.1983° |
| revolutions per day: | 11.82564286 |
| mean anomaly at epoch: | 42.6873° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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