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 55819U 26145.39902725 +.00000000 +00000-0 +20255-3 0 00003
2 55819 87.9158 309.4914 0001384 91.5884 268.5408 13.19726333 00
| Epoch (UTC): | 25 May 2026 09:34:35 |
| Eccentricity: | 0.0001384 |
| inclination: | 87.9158° |
| perigee height: | 1185 km |
| apogee height: | 1187 km |
| right ascension of ascending node: | 309.4914° |
| argument of perigee: | 91.5884° |
| revolutions per day: | 13.19726333 |
| mean anomaly at epoch: | 268.5408° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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