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 65832U 26143.27861280 +.00000000 +00000-0 +68952-3 0 00000
2 65832 53.1620 101.8507 0001798 139.0441 221.0695 15.30223797 06
| Epoch (UTC): | 23 May 2026 06:41:12 |
| Eccentricity: | 0.0001798 |
| inclination: | 53.1620° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 101.8507° |
| argument of perigee: | 139.0441° |
| revolutions per day: | 15.30223797 |
| mean anomaly at epoch: | 221.0695° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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