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 53604U 26145.57154896 +.00000000 +00000-0 +25359-4 0 00002
2 53604 53.2146 253.8419 0001330 85.2906 274.8238 15.08840419 04
| Epoch (UTC): | 25 May 2026 13:43:01 |
| Eccentricity: | 0.0001330 |
| inclination: | 53.2146° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 253.8419° |
| argument of perigee: | 85.2906° |
| revolutions per day: | 15.08840419 |
| mean anomaly at epoch: | 274.8238° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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