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 52309U 26145.14376875 +.00000000 +00000-0 +37764-4 0 00002
2 52309 53.2138 105.9009 0000937 63.6918 296.4171 15.08851342 06
| Epoch (UTC): | 25 May 2026 03:27:01 |
| Eccentricity: | 0.0000937 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 105.9009° |
| argument of perigee: | 63.6918° |
| revolutions per day: | 15.08851342 |
| mean anomaly at epoch: | 296.4171° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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