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 25198.51412198 .00000336 00000-0 39740-4 0 9990
2 21398 82.5229 356.0994 0019822 216.1534 143.8341 14.81570864840609
| Epoch (UTC): | 17 July 2025 12:20:20 |
| Eccentricity: | 0.0019822 |
| inclination: | 82.5229° |
| perigee height: | 610 km |
| apogee height: | 638 km |
| right ascension of ascending node: | 356.0994° |
| argument of perigee: | 216.1534° |
| revolutions per day: | 14.81570864 |
| mean anomaly at epoch: | 143.8341° |
| orbit number at epoch: | 84060 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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