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 44387U 26139.51390683 +.00000000 +00000-0 +13444-3 0 00004
2 44387 98.9136 126.3784 0002375 92.3586 267.7864 14.24357825 06
| Epoch (UTC): | 19 May 2026 12:20:01 |
| Eccentricity: | 0.0002375 |
| inclination: | 98.9136° |
| perigee height: | 809 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 126.3784° |
| argument of perigee: | 92.3586° |
| revolutions per day: | 14.24357825 |
| mean anomaly at epoch: | 267.7864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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