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 26065.27524433 +.00000000 +00000-0 +65482-4 0 00006
2 25774 51.5284 268.0026 0374080 236.7831 298.7072 13.46767063 06
| Epoch (UTC): | 06 March 2026 06:36:21 |
| Eccentricity: | 0.0374080 |
| inclination: | 51.5284° |
| perigee height: | 805 km |
| apogee height: | 1363 km |
| right ascension of ascending node: | 268.0026° |
| argument of perigee: | 236.7831° |
| revolutions per day: | 13.46767063 |
| mean anomaly at epoch: | 298.7072° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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