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 51791U 26145.02784682 +.00000000 +00000-0 +10543-4 0 00008
2 51791 53.2135 6.4255 0001568 96.4997 263.6174 15.08843307 08
| Epoch (UTC): | 25 May 2026 00:40:05 |
| Eccentricity: | 0.0001568 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 6.4255° |
| argument of perigee: | 96.4997° |
| revolutions per day: | 15.08843307 |
| mean anomaly at epoch: | 263.6174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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