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 40874U 26144.85983779 +.00000000 +00000-0 +00000-0 0 00009
2 40874 0.0097 314.0541 0000602 28.1116 154.3402 1.00271651 08
| Epoch (UTC): | 24 May 2026 20:38:09 |
| Eccentricity: | 0.0000602 |
| inclination: | 0.0097° |
| perigee height: | 35784 km |
| apogee height: | 35789 km |
| right ascension of ascending node: | 314.0541° |
| argument of perigee: | 28.1116° |
| revolutions per day: | 1.00271651 |
| mean anomaly at epoch: | 154.3402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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