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 40024U 14033Q 25162.71422327 .00008121 00000-0 39837-3 0 9990
2 40024 98.0895 160.7867 0005810 46.3583 313.8130 15.18393689597530
| Epoch (UTC): | 11 June 2025 17:08:28 |
| Eccentricity: | 0.0005810 |
| inclination: | 98.0895° |
| perigee height: | 506 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 160.7867° |
| argument of perigee: | 46.3583° |
| revolutions per day: | 15.18393689 |
| mean anomaly at epoch: | 313.8130° |
| orbit number at epoch: | 59753 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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