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 52372U 26145.46576983 +.00000000 +00000-0 +66651-5 0 00007
2 52372 53.2108 204.4593 0000965 62.7794 297.3296 15.08834224 07
| Epoch (UTC): | 25 May 2026 11:10:42 |
| Eccentricity: | 0.0000965 |
| inclination: | 53.2108° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 204.4593° |
| argument of perigee: | 62.7794° |
| revolutions per day: | 15.08834224 |
| mean anomaly at epoch: | 297.3296° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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