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 52153U 26145.62318550 +.00000000 +00000-0 +64874-4 0 00000
2 52153 97.5873 183.9917 0008982 254.4896 105.5335 14.97131241 05
| Epoch (UTC): | 25 May 2026 14:57:23 |
| Eccentricity: | 0.0008982 |
| inclination: | 97.5873° |
| perigee height: | 570 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 183.9917° |
| argument of perigee: | 254.4896° |
| revolutions per day: | 14.97131241 |
| mean anomaly at epoch: | 105.5335° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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