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 25774U 26074.44459897 +.00000000 +00000-0 +56249-4 0 00007
2 25774 51.5286 235.0993 0373954 261.5219 115.0176 13.46768176 02
| Epoch (UTC): | 15 March 2026 10:40:13 |
| Eccentricity: | 0.0373954 |
| inclination: | 51.5286° |
| perigee height: | 805 km |
| apogee height: | 1363 km |
| right ascension of ascending node: | 235.0993° |
| argument of perigee: | 261.5219° |
| revolutions per day: | 13.46768176 |
| mean anomaly at epoch: | 115.0176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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