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 53698U 26145.62838057 +.00000000 +00000-0 +36281-4 0 00005
2 53698 98.1811 153.8298 0001241 179.9654 180.1546 14.58716238 06
| Epoch (UTC): | 25 May 2026 15:04:52 |
| Eccentricity: | 0.0001241 |
| inclination: | 98.1811° |
| perigee height: | 696 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 153.8298° |
| argument of perigee: | 179.9654° |
| revolutions per day: | 14.58716238 |
| mean anomaly at epoch: | 180.1546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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