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 62362U 26145.48797205 +.00000000 +00000-0 +00000-0 0 00002
2 62362 0.0698 352.8814 0006062 68.5209 298.6583 5.00115177 07
| Epoch (UTC): | 25 May 2026 11:42:40 |
| Eccentricity: | 0.0006062 |
| inclination: | 0.0698° |
| perigee height: | 8057 km |
| apogee height: | 8075 km |
| right ascension of ascending node: | 352.8814° |
| argument of perigee: | 68.5209° |
| revolutions per day: | 5.00115177 |
| mean anomaly at epoch: | 298.6583° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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