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 62389U 26145.63267016 +.00000000 +00000-0 +13712-3 0 00007
2 62389 44.9968 117.4343 0000059 357.6573 2.4304 15.13040953 07
| Epoch (UTC): | 25 May 2026 15:11:02 |
| Eccentricity: | 0.0000059 |
| inclination: | 44.9968° |
| perigee height: | 527 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 117.4343° |
| argument of perigee: | 357.6573° |
| revolutions per day: | 15.13040953 |
| mean anomaly at epoch: | 2.4304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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