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 26158.61732897 +.00000000 +00000-0 +17737-3 0 00003
2 06155 35.0001 138.6446 0032984 46.6843 313.6600 14.77902216 05
| Epoch (UTC): | 07 June 2026 14:48:57 |
| Eccentricity: | 0.0032984 |
| inclination: | 35.0001° |
| perigee height: | 613 km |
| apogee height: | 659 km |
| right ascension of ascending node: | 138.6446° |
| argument of perigee: | 46.6843° |
| revolutions per day: | 14.77902216 |
| mean anomaly at epoch: | 313.6600° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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