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 63267U 26145.03459421 +.00000000 +00000-0 +13586-2 0 00008
2 63267 43.0049 12.3058 0002866 260.0336 100.0209 15.70901179 09
| Epoch (UTC): | 25 May 2026 00:49:48 |
| Eccentricity: | 0.0002866 |
| inclination: | 43.0049° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 12.3058° |
| argument of perigee: | 260.0336° |
| revolutions per day: | 15.70901179 |
| mean anomaly at epoch: | 100.0209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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