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 52674U 26145.66668980 +.00000000 +00000-0 +15268-2 0 00008
2 52674 53.2167 162.7885 0000755 64.8814 277.0539 15.37725020 00
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0000755 |
| inclination: | 53.2167° |
| perigee height: | 452 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 162.7885° |
| argument of perigee: | 64.8814° |
| revolutions per day: | 15.37725020 |
| mean anomaly at epoch: | 277.0539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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