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 54772U 26145.10514716 +.00000000 +00000-0 +20841-4 0 00000
2 54772 53.2124 46.2216 0001391 81.4772 278.6378 15.08838218 03
| Epoch (UTC): | 25 May 2026 02:31:24 |
| Eccentricity: | 0.0001391 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 46.2216° |
| argument of perigee: | 81.4772° |
| revolutions per day: | 15.08838218 |
| mean anomaly at epoch: | 278.6378° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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