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 53210U 26145.43718701 +.00000000 +00000-0 -15378-4 0 00002
2 53210 97.4536 205.3577 0001801 137.5326 222.6040 15.05647334 07
| Epoch (UTC): | 25 May 2026 10:29:32 |
| Eccentricity: | 0.0001801 |
| inclination: | 97.4536° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 205.3577° |
| argument of perigee: | 137.5326° |
| revolutions per day: | 15.05647334 |
| mean anomaly at epoch: | 222.6040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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