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 04420U 26039.60026744 +.00000000 +00000-0 +71010-4 0 00005
2 04420 81.2314 122.8373 0085759 275.3035 83.8357 14.12602848 06
| Epoch (UTC): | 08 February 2026 14:24:23 |
| Eccentricity: | 0.0085759 |
| inclination: | 81.2314° |
| perigee height: | 788 km |
| apogee height: | 912 km |
| right ascension of ascending node: | 122.8373° |
| argument of perigee: | 275.3035° |
| revolutions per day: | 14.12602848 |
| mean anomaly at epoch: | 83.8357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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