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 62440U 26145.56854959 +.00000000 +00000-0 +32759-3 0 00007
2 62440 53.1595 337.8722 0001007 97.2061 262.9055 15.30202289 02
| Epoch (UTC): | 25 May 2026 13:38:42 |
| Eccentricity: | 0.0001007 |
| inclination: | 53.1595° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 337.8722° |
| argument of perigee: | 97.2061° |
| revolutions per day: | 15.30202289 |
| mean anomaly at epoch: | 262.9055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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