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 26020.17509288 +.00000000 +00000-0 +38548-3 0 00004
2 25544 51.6334 312.1983 0007785 38.3265 321.8276 15.49442598 05
| Epoch (UTC): | 20 January 2026 04:12:08 |
| Eccentricity: | 0.0007785 |
| inclination: | 51.6334° |
| perigee height: | 413 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 312.1983° |
| argument of perigee: | 38.3265° |
| revolutions per day: | 15.49442598 |
| mean anomaly at epoch: | 321.8276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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