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 63867U 26145.40795471 +.00000000 +00000-0 +67359-3 0 00001
2 63867 70.0049 41.0751 0002657 267.7728 92.3127 14.98336283 00
| Epoch (UTC): | 25 May 2026 09:47:27 |
| Eccentricity: | 0.0002657 |
| inclination: | 70.0049° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.0751° |
| argument of perigee: | 267.7728° |
| revolutions per day: | 14.98336283 |
| mean anomaly at epoch: | 92.3127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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