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 19025U 26087.69366073 +.00000000 +00000-0 +14977-2 0 00003
2 19025 82.7065 185.1733 0021751 49.2068 311.1001 14.30635736 05
| Epoch (UTC): | 28 March 2026 16:38:52 |
| Eccentricity: | 0.0021751 |
| inclination: | 82.7065° |
| perigee height: | 774 km |
| apogee height: | 805 km |
| right ascension of ascending node: | 185.1733° |
| argument of perigee: | 49.2068° |
| revolutions per day: | 14.30635736 |
| mean anomaly at epoch: | 311.1001° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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