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 40062U 26145.46959990 +.00000000 +00000-0 +10897-2 0 00001
2 40062 82.5100 321.7755 0022779 203.0886 156.9172 12.42950622 08
| Epoch (UTC): | 25 May 2026 11:16:13 |
| Eccentricity: | 0.0022779 |
| inclination: | 82.5100° |
| perigee height: | 1476 km |
| apogee height: | 1512 km |
| right ascension of ascending node: | 321.7755° |
| argument of perigee: | 203.0886° |
| revolutions per day: | 12.42950622 |
| mean anomaly at epoch: | 156.9172° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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