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 62382U 26145.12452236 +.00000000 +00000-0 +21298-3 0 00002
2 62382 44.9952 54.8463 0003134 78.4500 281.6736 15.29976771 08
| Epoch (UTC): | 25 May 2026 02:59:18 |
| Eccentricity: | 0.0003134 |
| inclination: | 44.9952° |
| perigee height: | 474 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 54.8463° |
| argument of perigee: | 78.4500° |
| revolutions per day: | 15.29976771 |
| mean anomaly at epoch: | 281.6736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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