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 59051U 26040.58236882 +.00000000 +00000-0 +39191-4 0 00004
2 59051 98.6854 1.5952 0007088 170.4148 189.7166 14.22412644 00
| Epoch (UTC): | 09 February 2026 13:58:36 |
| Eccentricity: | 0.0007088 |
| inclination: | 98.6854° |
| perigee height: | 812 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 1.5952° |
| argument of perigee: | 170.4148° |
| revolutions per day: | 14.22412644 |
| mean anomaly at epoch: | 189.7166° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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