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 53202U 26145.40808426 +.00000000 +00000-0 +86794-4 0 00003
2 53202 97.4466 206.4838 0002563 123.1350 237.0124 15.05644424 06
| Epoch (UTC): | 25 May 2026 09:47:38 |
| Eccentricity: | 0.0002563 |
| inclination: | 97.4466° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 206.4838° |
| argument of perigee: | 123.1350° |
| revolutions per day: | 15.05644424 |
| mean anomaly at epoch: | 237.0124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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