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 63796U 26144.88853766 +.00000000 +00000-0 +73332-3 0 00003
2 63796 43.0008 342.3835 0001323 272.8724 87.1976 15.27595650 00
| Epoch (UTC): | 24 May 2026 21:19:29 |
| Eccentricity: | 0.0001323 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.3835° |
| argument of perigee: | 272.8724° |
| revolutions per day: | 15.27595650 |
| mean anomaly at epoch: | 87.1976° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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