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 65698U 26144.85012610 +.00000000 +00000-0 +77118-3 0 00004
2 65698 53.1604 351.9434 0001193 86.5754 273.5383 15.30210861 01
| Epoch (UTC): | 24 May 2026 20:24:10 |
| Eccentricity: | 0.0001193 |
| inclination: | 53.1604° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 351.9434° |
| argument of perigee: | 86.5754° |
| revolutions per day: | 15.30210861 |
| mean anomaly at epoch: | 273.5383° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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