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 52332U 26145.49800426 +.00000000 +00000-0 -57105-4 0 00002
2 52332 53.2131 224.3257 0000984 65.8030 294.3065 15.08843474 03
| Epoch (UTC): | 25 May 2026 11:57:07 |
| Eccentricity: | 0.0000984 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 224.3257° |
| argument of perigee: | 65.8030° |
| revolutions per day: | 15.08843474 |
| mean anomaly at epoch: | 294.3065° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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