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 61532U 26145.39527509 +.00000000 +00000-0 +69128-5 0 00009
2 61532 53.1591 218.2151 0001067 109.6284 250.4849 15.69701780 03
| Epoch (UTC): | 25 May 2026 09:29:11 |
| Eccentricity: | 0.0001067 |
| inclination: | 53.1591° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 218.2151° |
| argument of perigee: | 109.6284° |
| revolutions per day: | 15.69701780 |
| mean anomaly at epoch: | 250.4849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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