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 40749U 26143.83404854 +.00000000 +00000-0 +00000-0 0 00009
2 40749 54.8897 302.8719 0003923 58.3159 301.7019 1.86254827 09
| Epoch (UTC): | 23 May 2026 20:01:01 |
| Eccentricity: | 0.0003923 |
| inclination: | 54.8897° |
| perigee height: | 21515 km |
| apogee height: | 21537 km |
| right ascension of ascending node: | 302.8719° |
| argument of perigee: | 58.3159° |
| revolutions per day: | 1.86254827 |
| mean anomaly at epoch: | 301.7019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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