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 52552U 26145.37562781 +.00000000 +00000-0 +68814-4 0 00000
2 52552 53.2111 145.0147 0001130 74.8828 285.2289 15.08839316 08
| Epoch (UTC): | 25 May 2026 09:00:54 |
| Eccentricity: | 0.0001130 |
| inclination: | 53.2111° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 145.0147° |
| argument of perigee: | 74.8828° |
| revolutions per day: | 15.08839316 |
| mean anomaly at epoch: | 285.2289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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