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 00058U 26040.28825105 +.00000000 +00000-0 +17655-4 0 00007
2 00058 28.3286 68.7089 0164749 228.7072 129.9182 13.46424141 03
| Epoch (UTC): | 09 February 2026 06:55:04 |
| Eccentricity: | 0.0164749 |
| inclination: | 28.3286° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 68.7089° |
| argument of perigee: | 228.7072° |
| revolutions per day: | 13.46424141 |
| mean anomaly at epoch: | 129.9182° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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