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 62006U 26145.61711272 +.00000000 +00000-0 +00000-0 0 00002
2 62006 0.0193 307.3167 0001536 150.1074 164.3370 1.00271506 05
| Epoch (UTC): | 25 May 2026 14:48:38 |
| Eccentricity: | 0.0001536 |
| inclination: | 0.0193° |
| perigee height: | 35780 km |
| apogee height: | 35793 km |
| right ascension of ascending node: | 307.3167° |
| argument of perigee: | 150.1074° |
| revolutions per day: | 1.00271506 |
| mean anomaly at epoch: | 164.3370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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