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 52293U 26145.33516594 +.00000000 +00000-0 +43236-4 0 00000
2 52293 53.2132 115.0531 0001439 85.3530 274.7627 15.08836302 07
| Epoch (UTC): | 25 May 2026 08:02:38 |
| Eccentricity: | 0.0001439 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 115.0531° |
| argument of perigee: | 85.3530° |
| revolutions per day: | 15.08836302 |
| mean anomaly at epoch: | 274.7627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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