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 63937U 26145.53792111 +.00000000 +00000-0 -20264-3 0 00006
2 63937 70.0012 80.6916 0002315 273.3726 86.7169 14.98328838 02
| Epoch (UTC): | 25 May 2026 12:54:36 |
| Eccentricity: | 0.0002315 |
| inclination: | 70.0012° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 80.6916° |
| argument of perigee: | 273.3726° |
| revolutions per day: | 14.98328838 |
| mean anomaly at epoch: | 86.7169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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