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 26076.89347623 +.00000000 +00000-0 +11171-3 0 00008
2 40059 98.2004 19.6155 0001359 95.3844 264.7509 14.57103976 07
| Epoch (UTC): | 17 March 2026 21:26:36 |
| Eccentricity: | 0.0001359 |
| inclination: | 98.2004° |
| perigee height: | 702 km |
| apogee height: | 704 km |
| right ascension of ascending node: | 19.6155° |
| argument of perigee: | 95.3844° |
| revolutions per day: | 14.57103976 |
| mean anomaly at epoch: | 264.7509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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