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 62452U 26144.97766425 +.00000000 +00000-0 +43826-3 0 00001
2 62452 53.1603 341.2915 0001215 80.9543 279.1595 15.30209810 09
| Epoch (UTC): | 24 May 2026 23:27:50 |
| Eccentricity: | 0.0001215 |
| inclination: | 53.1603° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 341.2915° |
| argument of perigee: | 80.9543° |
| revolutions per day: | 15.30209810 |
| mean anomaly at epoch: | 279.1595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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