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 62374U 26145.54280769 +.00000000 +00000-0 +00000-0 0 00004
2 62374 0.7190 297.1786 0002174 71.6187 216.2145 1.00268519 08
| Epoch (UTC): | 25 May 2026 13:01:38 |
| Eccentricity: | 0.0002174 |
| inclination: | 0.7190° |
| perigee height: | 35778 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 297.1786° |
| argument of perigee: | 71.6187° |
| revolutions per day: | 1.00268519 |
| mean anomaly at epoch: | 216.2145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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