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 40344U 14081A 25165.74056490 0.00000000 00000-0 00000-0 0 06
2 40344 62.9350 118.6321 6893710 270.8769 89.1231 2.00611587 01
| Epoch (UTC): | 14 June 2025 17:46:24 |
| Eccentricity: | 0.6893710 |
| inclination: | 62.9350° |
| perigee height: | 1871 km |
| apogee height: | 38484 km |
| right ascension of ascending node: | 118.6321° |
| argument of perigee: | 270.8769° |
| revolutions per day: | 2.00611587 |
| mean anomaly at epoch: | 89.1231° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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