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 49752U 26145.31678032 +.00000000 +00000-0 -18981-5 0 00001
2 49752 53.2118 155.1378 0001421 71.5792 288.5355 15.08835992 04
| Epoch (UTC): | 25 May 2026 07:36:09 |
| Eccentricity: | 0.0001421 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 155.1378° |
| argument of perigee: | 71.5792° |
| revolutions per day: | 15.08835992 |
| mean anomaly at epoch: | 288.5355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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