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 53022U 26145.25278949 +.00000000 +00000-0 +51270-4 0 00008
2 53022 53.2134 100.4122 0001577 91.6518 268.4655 15.08837504 09
| Epoch (UTC): | 25 May 2026 06:04:01 |
| Eccentricity: | 0.0001577 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 100.4122° |
| argument of perigee: | 91.6518° |
| revolutions per day: | 15.08837504 |
| mean anomaly at epoch: | 268.4655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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