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 26550U 26063.90692166 +.00000000 +00000-0 +38009-4 0 00001
2 26550 64.5613 234.3221 0506355 55.6947 309.0971 13.82060576 09
| Epoch (UTC): | 04 March 2026 21:45:58 |
| Eccentricity: | 0.0506355 |
| inclination: | 64.5613° |
| perigee height: | 585 km |
| apogee height: | 1328 km |
| right ascension of ascending node: | 234.3221° |
| argument of perigee: | 55.6947° |
| revolutions per day: | 13.82060576 |
| mean anomaly at epoch: | 309.0971° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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