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 26072.84048773 +.00000000 +00000-0 +72318-4 0 00001
2 25774 51.5284 240.8554 0373961 257.1940 257.7091 13.46767958 04
| Epoch (UTC): | 13 March 2026 20:10:18 |
| Eccentricity: | 0.0373961 |
| inclination: | 51.5284° |
| perigee height: | 805 km |
| apogee height: | 1363 km |
| right ascension of ascending node: | 240.8554° |
| argument of perigee: | 257.1940° |
| revolutions per day: | 13.46767958 |
| mean anomaly at epoch: | 257.7091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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