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 52667U 26145.36413926 +.00000000 +00000-0 -24220-3 0 00005
2 52667 53.2135 169.9174 0001199 65.1847 294.9269 15.08807473 09
| Epoch (UTC): | 25 May 2026 08:44:21 |
| Eccentricity: | 0.0001199 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 169.9174° |
| argument of perigee: | 65.1847° |
| revolutions per day: | 15.08807473 |
| mean anomaly at epoch: | 294.9269° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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