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 62339U 26143.66691068 +.00000000 +00000-0 +00000-0 0 00004
2 62339 54.8596 335.1744 0017374 3.8345 179.6490 2.00571082 05
| Epoch (UTC): | 23 May 2026 16:00:21 |
| Eccentricity: | 0.0017374 |
| inclination: | 54.8596° |
| perigee height: | 20135 km |
| apogee height: | 20228 km |
| right ascension of ascending node: | 335.1744° |
| argument of perigee: | 3.8345° |
| revolutions per day: | 2.00571082 |
| mean anomaly at epoch: | 179.6490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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