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 62384U 26145.38832902 +.00000000 +00000-0 +17327-3 0 00002
2 62384 44.9972 119.0812 0001282 286.4761 73.5975 15.12778750 08
| Epoch (UTC): | 25 May 2026 09:19:11 |
| Eccentricity: | 0.0001282 |
| inclination: | 44.9972° |
| perigee height: | 527 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 119.0812° |
| argument of perigee: | 286.4761° |
| revolutions per day: | 15.12778750 |
| mean anomaly at epoch: | 73.5975° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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