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 06153U 26032.42138877 +.00000000 +00000-0 +94035-4 0 00006
2 06153 35.0049 143.9435 0007021 228.3055 188.1812 14.59963213 04
| Epoch (UTC): | 01 February 2026 10:06:47 |
| Eccentricity: | 0.0007021 |
| inclination: | 35.0049° |
| perigee height: | 688 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 143.9435° |
| argument of perigee: | 228.3055° |
| revolutions per day: | 14.59963213 |
| mean anomaly at epoch: | 188.1812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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