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 40697U 26107.93500412 +.00000000 +00000-0 -67036-4 0 00006
2 40697 98.5636 183.6507 0001338 89.1368 270.9969 14.30819874 02
| Epoch (UTC): | 17 April 2026 22:26:24 |
| Eccentricity: | 0.0001338 |
| inclination: | 98.5636° |
| perigee height: | 788 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 183.6507° |
| argument of perigee: | 89.1368° |
| revolutions per day: | 14.30819874 |
| mean anomaly at epoch: | 270.9969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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