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 42808U 26145.30896904 +.00000000 +00000-0 +18248-4 0 00009
2 42808 86.3983 3.1580 0002254 83.8627 276.2825 14.34218103 04
| Epoch (UTC): | 25 May 2026 07:24:54 |
| Eccentricity: | 0.0002254 |
| inclination: | 86.3983° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 3.1580° |
| argument of perigee: | 83.8627° |
| revolutions per day: | 14.34218103 |
| mean anomaly at epoch: | 276.2825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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