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 26019.29980987 +.00000000 +00000-0 +13777-3 0 00008
2 06155 35.0005 235.1627 0034413 313.8425 45.9434 14.77517080 08
| Epoch (UTC): | 19 January 2026 07:11:43 |
| Eccentricity: | 0.0034413 |
| inclination: | 35.0005° |
| perigee height: | 613 km |
| apogee height: | 661 km |
| right ascension of ascending node: | 235.1627° |
| argument of perigee: | 313.8425° |
| revolutions per day: | 14.77517080 |
| mean anomaly at epoch: | 45.9434° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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