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 26145.52327874 +.00000000 +00000-0 +96640-3 0 00004
2 40553 82.4913 46.2298 0016237 38.5464 321.6772 12.42890867 01
| Epoch (UTC): | 25 May 2026 12:33:31 |
| Eccentricity: | 0.0016237 |
| inclination: | 82.4913° |
| perigee height: | 1482 km |
| apogee height: | 1507 km |
| right ascension of ascending node: | 46.2298° |
| argument of perigee: | 38.5464° |
| revolutions per day: | 12.42890867 |
| mean anomaly at epoch: | 321.6772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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