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 25544U 26103.16688154 +.00000000 +00000-0 +96801-4 0 00002
2 25544 51.6321 261.8843 0006463 306.5385 53.5008 15.48891757 07
| Epoch (UTC): | 13 April 2026 04:00:18 |
| Eccentricity: | 0.0006463 |
| inclination: | 51.6321° |
| perigee height: | 416 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 261.8843° |
| argument of perigee: | 306.5385° |
| revolutions per day: | 15.48891757 |
| mean anomaly at epoch: | 53.5008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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