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 00154U 26018.82956080 +.00000000 +00000-0 +14600-3 0 00002
2 00154 66.6571 169.5948 0076412 119.5447 241.3284 14.06226311 06
| Epoch (UTC): | 18 January 2026 19:54:34 |
| Eccentricity: | 0.0076412 |
| inclination: | 66.6571° |
| perigee height: | 817 km |
| apogee height: | 928 km |
| right ascension of ascending node: | 169.5948° |
| argument of perigee: | 119.5447° |
| revolutions per day: | 14.06226311 |
| mean anomaly at epoch: | 241.3284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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