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 26075.77378586 +.00000000 +00000-0 +30341-4 0 00007
2 26550 64.5630 203.0335 0507124 52.7088 311.9091 13.82064444 09
| Epoch (UTC): | 16 March 2026 18:34:15 |
| Eccentricity: | 0.0507124 |
| inclination: | 64.5630° |
| perigee height: | 585 km |
| apogee height: | 1329 km |
| right ascension of ascending node: | 203.0335° |
| argument of perigee: | 52.7088° |
| revolutions per day: | 13.82064444 |
| mean anomaly at epoch: | 311.9091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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