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 53201U 26145.66668980 +.00000000 +00000-0 +23644-2 0 00002
2 53201 97.6008 207.5843 0001629 89.9334 307.0125 15.22273061 03
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001629 |
| inclination: | 97.6008° |
| perigee height: | 498 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 207.5843° |
| argument of perigee: | 89.9334° |
| revolutions per day: | 15.22273061 |
| mean anomaly at epoch: | 307.0125° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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