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 21809U 91076E 25196.70971360 .00002370 00000-0 21548-3 0 9994
2 21809 63.3017 334.1256 0900632 68.3141 301.1287 13.53544320 58677
| Epoch (UTC): | 15 July 2025 17:01:59 |
| Eccentricity: | 0.0900632 |
| inclination: | 63.3017° |
| perigee height: | 389 km |
| apogee height: | 1729 km |
| right ascension of ascending node: | 334.1256° |
| argument of perigee: | 68.3141° |
| revolutions per day: | 13.53544320 |
| mean anomaly at epoch: | 301.1287° |
| orbit number at epoch: | 5867 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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