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 52746U 26145.56198316 +.00000000 +00000-0 +19820-3 0 00007
2 52746 97.6492 289.2343 0006589 174.1020 186.0301 15.34006644 09
| Epoch (UTC): | 25 May 2026 13:29:15 |
| Eccentricity: | 0.0006589 |
| inclination: | 97.6492° |
| perigee height: | 459 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 289.2343° |
| argument of perigee: | 174.1020° |
| revolutions per day: | 15.34006644 |
| mean anomaly at epoch: | 186.0301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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