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 62329U 26145.59064868 +.00000000 +00000-0 +14667-3 0 00006
2 62329 86.4952 350.5850 0001448 82.9841 277.1458 13.24408433 09
| Epoch (UTC): | 25 May 2026 14:10:32 |
| Eccentricity: | 0.0001448 |
| inclination: | 86.4952° |
| perigee height: | 1167 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 350.5850° |
| argument of perigee: | 82.9841° |
| revolutions per day: | 13.24408433 |
| mean anomaly at epoch: | 277.1458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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