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 52267U 26145.20448939 +.00000000 +00000-0 +64652-4 0 00009
2 52267 53.2123 125.6377 0001017 68.2643 291.8458 15.08847043 06
| Epoch (UTC): | 25 May 2026 04:54:27 |
| Eccentricity: | 0.0001017 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 125.6377° |
| argument of perigee: | 68.2643° |
| revolutions per day: | 15.08847043 |
| mean anomaly at epoch: | 291.8458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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