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 data is extracted from the following two-line orbital elements,
1 40061U 14036A 25110.95067519 .00000021 00000-0 78590-4 0 9992
2 40061 82.5134 209.8432 0028893 352.2485 7.8144 12.42967193489990
| Epoch (UTC): | 20 April 2025 22:48:58 |
| Eccentricity: | 0.0028893 |
| inclination: | 82.5134° |
| perigee height: | 1471 km |
| apogee height: | 1517 km |
| right ascension of ascending node: | 209.8432° |
| argument of perigee: | 352.2485° |
| revolutions per day: | 12.42967193 |
| mean anomaly at epoch: | 7.8144° |
| orbit number at epoch: | 48999 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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