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 51773U 26145.57803920 +.00000000 +00000-0 -98395-5 0 00008
2 51773 53.2131 353.9247 0001206 93.1630 266.9501 15.08839164 08
| Epoch (UTC): | 25 May 2026 13:52:22 |
| Eccentricity: | 0.0001206 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 353.9247° |
| argument of perigee: | 93.1630° |
| revolutions per day: | 15.08839164 |
| mean anomaly at epoch: | 266.9501° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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