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 62167U 26145.48451779 +.00000000 +00000-0 +31825-3 0 00000
2 62167 70.0010 331.0109 0002706 263.3375 96.7476 14.98317591 00
| Epoch (UTC): | 25 May 2026 11:37:42 |
| Eccentricity: | 0.0002706 |
| inclination: | 70.0010° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 331.0109° |
| argument of perigee: | 263.3375° |
| revolutions per day: | 14.98317591 |
| mean anomaly at epoch: | 96.7476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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