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 53206U 26145.41361544 +.00000000 +00000-0 -14310-3 0 00008
2 53206 97.4463 206.4584 0002333 129.6948 230.4485 15.05658112 00
| Epoch (UTC): | 25 May 2026 09:55:36 |
| Eccentricity: | 0.0002333 |
| inclination: | 97.4463° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 206.4584° |
| argument of perigee: | 129.6948° |
| revolutions per day: | 15.05658112 |
| mean anomaly at epoch: | 230.4485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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