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 53219U 26145.12563869 +.00000000 +00000-0 -44010-3 0 00004
2 53219 97.4515 206.1745 0000743 87.1330 272.9982 15.05658161 01
| Epoch (UTC): | 25 May 2026 03:00:55 |
| Eccentricity: | 0.0000743 |
| inclination: | 97.4515° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 206.1745° |
| argument of perigee: | 87.1330° |
| revolutions per day: | 15.05658161 |
| mean anomaly at epoch: | 272.9982° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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