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 54062U 26145.32455221 +.00000000 +00000-0 -70122-4 0 00009
2 54062 53.2142 0.0620 0001177 68.5193 291.5925 15.08844413 03
| Epoch (UTC): | 25 May 2026 07:47:21 |
| Eccentricity: | 0.0001177 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 0.0620° |
| argument of perigee: | 68.5193° |
| revolutions per day: | 15.08844413 |
| mean anomaly at epoch: | 291.5925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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