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 40553U 26106.96528706 +.00000000 +00000-0 +26391-3 0 00002
2 40553 82.4865 70.2410 0016061 117.1344 243.1376 12.42889670 04
| Epoch (UTC): | 16 April 2026 23:10:00 |
| Eccentricity: | 0.0016061 |
| inclination: | 82.4865° |
| perigee height: | 1482 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 70.2410° |
| argument of perigee: | 117.1344° |
| revolutions per day: | 12.42889670 |
| mean anomaly at epoch: | 243.1376° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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