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 25132.56203443 .00021498 00000-0 80241-3 0 9990
2 40021 98.0958 144.4908 0010649 65.0635 295.1707 15.27374750594047
| Epoch (UTC): | 12 May 2025 13:29:19 |
| Eccentricity: | 0.0010649 |
| inclination: | 98.0958° |
| perigee height: | 476 km |
| apogee height: | 491 km |
| right ascension of ascending node: | 144.4908° |
| argument of perigee: | 65.0635° |
| revolutions per day: | 15.27374750 |
| mean anomaly at epoch: | 295.1707° |
| orbit number at epoch: | 59404 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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