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 62274U 26145.52039617 +.00000000 +00000-0 +16560-2 0 00005
2 62274 42.9987 313.6879 0001259 291.3043 68.7690 15.70823228 02
| Epoch (UTC): | 25 May 2026 12:29:22 |
| Eccentricity: | 0.0001259 |
| inclination: | 42.9987° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 313.6879° |
| argument of perigee: | 291.3043° |
| revolutions per day: | 15.70823228 |
| mean anomaly at epoch: | 68.7690° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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