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 53100U 26145.58580845 +.00000000 +00000-0 +00000-0 0 00003
2 53100 0.6144 76.4956 0001854 308.0794 80.0633 1.00272532 04
| Epoch (UTC): | 25 May 2026 14:03:33 |
| Eccentricity: | 0.0001854 |
| inclination: | 0.6144° |
| perigee height: | 35779 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 76.4956° |
| argument of perigee: | 308.0794° |
| revolutions per day: | 1.00272532 |
| mean anomaly at epoch: | 80.0633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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