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 26104.22839075 +.00000000 +00000-0 +63017-4 0 00000
2 40553 82.4862 71.9464 0015977 122.8337 237.4284 12.42889395 06
| Epoch (UTC): | 14 April 2026 05:28:52 |
| Eccentricity: | 0.0015977 |
| inclination: | 82.4862° |
| perigee height: | 1482 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 71.9464° |
| argument of perigee: | 122.8337° |
| revolutions per day: | 12.42889395 |
| mean anomaly at epoch: | 237.4284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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