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 36592U 26145.58979513 +.00000000 +00000-0 +00000-0 0 00003
2 36592 0.0636 110.9366 0002148 82.0459 292.9190 1.00271409 07
| Epoch (UTC): | 25 May 2026 14:09:18 |
| Eccentricity: | 0.0002148 |
| inclination: | 0.0636° |
| perigee height: | 35778 km |
| apogee height: | 35796 km |
| right ascension of ascending node: | 110.9366° |
| argument of perigee: | 82.0459° |
| revolutions per day: | 1.00271409 |
| mean anomaly at epoch: | 292.9190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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