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 62028U 26145.52588512 +.00000000 +00000-0 +00000-0 0 00005
2 62028 0.0343 249.5771 0001981 174.4329 76.3760 1.00273355 09
| Epoch (UTC): | 25 May 2026 12:37:16 |
| Eccentricity: | 0.0001981 |
| inclination: | 0.0343° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 249.5771° |
| argument of perigee: | 174.4329° |
| revolutions per day: | 1.00273355 |
| mean anomaly at epoch: | 76.3760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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