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 53433U 26145.19574514 +.00000000 +00000-0 +62580-4 0 00000
2 53433 53.2137 120.6678 0001155 76.3609 283.7512 15.08842175 03
| Epoch (UTC): | 25 May 2026 04:41:52 |
| Eccentricity: | 0.0001155 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 120.6678° |
| argument of perigee: | 76.3609° |
| revolutions per day: | 15.08842175 |
| mean anomaly at epoch: | 283.7512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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