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 63242U 26144.94158257 +.00000000 +00000-0 +18238-3 0 00003
2 63242 97.3932 36.9839 0005412 265.1528 94.9090 15.21347451 05
| Epoch (UTC): | 24 May 2026 22:35:52 |
| Eccentricity: | 0.0005412 |
| inclination: | 97.3932° |
| perigee height: | 498 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 36.9839° |
| argument of perigee: | 265.1528° |
| revolutions per day: | 15.21347451 |
| mean anomaly at epoch: | 94.9090° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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