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 40021U 14033M 25172.50294041 .00014442 00000-0 51498-3 0 9995
2 40021 98.0943 187.8789 0006604 273.1472 86.9010 15.29007241600148
| Epoch (UTC): | 21 June 2025 12:04:14 |
| Eccentricity: | 0.0006604 |
| inclination: | 98.0943° |
| perigee height: | 474 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 187.8789° |
| argument of perigee: | 273.1472° |
| revolutions per day: | 15.29007241 |
| mean anomaly at epoch: | 86.9010° |
| orbit number at epoch: | 60014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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