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 26158.91310072 +.00000000 +00000-0 +57196-4 0 00008
2 26550 64.5633 343.8050 0513125 32.0712 331.0499 13.82099774 01
| Epoch (UTC): | 07 June 2026 21:54:51 |
| Eccentricity: | 0.0513125 |
| inclination: | 64.5633° |
| perigee height: | 580 km |
| apogee height: | 1333 km |
| right ascension of ascending node: | 343.8050° |
| argument of perigee: | 32.0712° |
| revolutions per day: | 13.82099774 |
| mean anomaly at epoch: | 331.0499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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