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 21398U 91039B 25197.90628278 .00000324 00000-0 38216-4 0 9994
2 21398 82.5229 356.6671 0019781 218.2660 141.7151 14.81570405819483
| Epoch (UTC): | 16 July 2025 21:45:02 |
| Eccentricity: | 0.0019781 |
| inclination: | 82.5229° |
| perigee height: | 610 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 356.6671° |
| argument of perigee: | 218.2660° |
| revolutions per day: | 14.81570405 |
| mean anomaly at epoch: | 141.7151° |
| orbit number at epoch: | 81948 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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