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 26075.88547127 +.00000000 +00000-0 +54636-4 0 00008
2 25774 51.5287 229.9292 0373951 265.4067 260.8886 13.46768397 00
| Epoch (UTC): | 16 March 2026 21:15:04 |
| Eccentricity: | 0.0373951 |
| inclination: | 51.5287° |
| perigee height: | 805 km |
| apogee height: | 1363 km |
| right ascension of ascending node: | 229.9292° |
| argument of perigee: | 265.4067° |
| revolutions per day: | 13.46768397 |
| mean anomaly at epoch: | 260.8886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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