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 06155U 26106.05627031 +.00000000 +00000-0 +93469-4 0 00004
2 06155 35.0013 86.7486 0033863 323.7629 36.0779 14.77789793 09
| Epoch (UTC): | 16 April 2026 01:21:01 |
| Eccentricity: | 0.0033863 |
| inclination: | 35.0013° |
| perigee height: | 613 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 86.7486° |
| argument of perigee: | 323.7629° |
| revolutions per day: | 14.77789793 |
| mean anomaly at epoch: | 36.0779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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