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 40014U 14033E 25163.19282729 .00004210 00000-0 25440-3 0 9992
2 40014 98.0741 229.9180 0030852 2.8363 357.3034 15.10891916599897
| Epoch (UTC): | 12 June 2025 04:37:40 |
| Eccentricity: | 0.0030852 |
| inclination: | 98.0741° |
| perigee height: | 512 km |
| apogee height: | 555 km |
| right ascension of ascending node: | 229.9180° |
| argument of perigee: | 2.8363° |
| revolutions per day: | 15.10891916 |
| mean anomaly at epoch: | 357.3034° |
| orbit number at epoch: | 59989 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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