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 32252U 26151.47947800 +.00000000 +00000-0 +00000-0 0 00001
2 32252 2.0381 82.2248 0002864 337.6458 251.9159 0.99340589 01
| Epoch (UTC): | 31 May 2026 11:30:26 |
| Eccentricity: | 0.0002864 |
| inclination: | 2.0381° |
| perigee height: | 36038 km |
| apogee height: | 36062 km |
| right ascension of ascending node: | 82.2248° |
| argument of perigee: | 337.6458° |
| revolutions per day: | 0.99340589 |
| mean anomaly at epoch: | 251.9159° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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