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 40552U 26145.63002976 +.00000000 +00000-0 +62537-3 0 00006
2 40552 82.4879 45.0455 0017354 52.5632 307.7023 12.42876567 02
| Epoch (UTC): | 25 May 2026 15:07:14 |
| Eccentricity: | 0.0017354 |
| inclination: | 82.4879° |
| perigee height: | 1481 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 45.0455° |
| argument of perigee: | 52.5632° |
| revolutions per day: | 12.42876567 |
| mean anomaly at epoch: | 307.7023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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