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 39420U 26032.13522181 +.00000000 +00000-0 +20310-3 0 00006
2 39420 97.7008 264.3142 0118771 89.9400 271.5418 14.71921900 00
| Epoch (UTC): | 01 February 2026 03:14:43 |
| Eccentricity: | 0.0118771 |
| inclination: | 97.7008° |
| perigee height: | 571 km |
| apogee height: | 738 km |
| right ascension of ascending node: | 264.3142° |
| argument of perigee: | 89.9400° |
| revolutions per day: | 14.71921900 |
| mean anomaly at epoch: | 271.5418° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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