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 52744U 26145.58028346 +.00000000 +00000-0 +19604-3 0 00002
2 52744 97.6655 291.9473 0006654 187.0723 173.0426 15.33996761 09
| Epoch (UTC): | 25 May 2026 13:55:36 |
| Eccentricity: | 0.0006654 |
| inclination: | 97.6655° |
| perigee height: | 459 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 291.9473° |
| argument of perigee: | 187.0723° |
| revolutions per day: | 15.33996761 |
| mean anomaly at epoch: | 173.0426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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