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 40059U 26073.87199705 +.00000000 +00000-0 +16783-3 0 00003
2 40059 98.1999 16.6412 0001318 94.6146 265.5203 14.57101189 08
| Epoch (UTC): | 14 March 2026 20:55:40 |
| Eccentricity: | 0.0001318 |
| inclination: | 98.1999° |
| perigee height: | 702 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 16.6412° |
| argument of perigee: | 94.6146° |
| revolutions per day: | 14.57101189 |
| mean anomaly at epoch: | 265.5203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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