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 53820U 26145.49755038 +.00000000 +00000-0 -48570-4 0 00009
2 53820 53.2130 319.5342 0001411 75.2525 284.8624 15.08835261 07
| Epoch (UTC): | 25 May 2026 11:56:28 |
| Eccentricity: | 0.0001411 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 319.5342° |
| argument of perigee: | 75.2525° |
| revolutions per day: | 15.08835261 |
| mean anomaly at epoch: | 284.8624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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