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 55919U 26145.31504757 +.00000000 +00000-0 +55070-4 0 00003
2 55919 69.9992 111.3082 0003630 267.9950 92.0793 14.98332128 02
| Epoch (UTC): | 25 May 2026 07:33:40 |
| Eccentricity: | 0.0003630 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 111.3082° |
| argument of perigee: | 267.9950° |
| revolutions per day: | 14.98332128 |
| mean anomaly at epoch: | 92.0793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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