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 25419U 26087.87936095 +.00000000 +00000-0 +43717-3 0 00009
2 25419 44.9949 263.2123 0002372 271.0350 89.0227 14.39948304 06
| Epoch (UTC): | 28 March 2026 21:06:16 |
| Eccentricity: | 0.0002372 |
| inclination: | 44.9949° |
| perigee height: | 757 km |
| apogee height: | 760 km |
| right ascension of ascending node: | 263.2123° |
| argument of perigee: | 271.0350° |
| revolutions per day: | 14.39948304 |
| mean anomaly at epoch: | 89.0227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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