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 63023U 26144.74540696 +.00000000 +00000-0 +85392-3 0 00005
2 63023 42.9993 266.3693 0001179 288.9983 71.0741 15.27606940 02
| Epoch (UTC): | 24 May 2026 17:53:23 |
| Eccentricity: | 0.0001179 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.3693° |
| argument of perigee: | 288.9983° |
| revolutions per day: | 15.27606940 |
| mean anomaly at epoch: | 71.0741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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