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 46553U 26145.38810338 +.00000000 +00000-0 +12364-2 0 00006
2 46553 53.0436 128.3350 0005644 42.3305 317.8137 15.47715899 00
| Epoch (UTC): | 25 May 2026 09:18:52 |
| Eccentricity: | 0.0005644 |
| inclination: | 53.0436° |
| perigee height: | 420 km |
| apogee height: | 427 km |
| right ascension of ascending node: | 128.3350° |
| argument of perigee: | 42.3305° |
| revolutions per day: | 15.47715899 |
| mean anomaly at epoch: | 317.8137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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