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 54792U 26145.45883897 +.00000000 +00000-0 +39482-3 0 00009
2 54792 53.2125 59.1297 0001541 98.2003 261.9164 15.08806100 01
| Epoch (UTC): | 25 May 2026 11:00:43 |
| Eccentricity: | 0.0001541 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 59.1297° |
| argument of perigee: | 98.2003° |
| revolutions per day: | 15.08806100 |
| mean anomaly at epoch: | 261.9164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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