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 21938U 92020B 25198.45037097 .00000100 00000-0 88387-4 0 9995
2 21938 82.9327 328.4639 0028013 232.7422 191.3569 13.75515434668795
| Epoch (UTC): | 17 July 2025 10:48:32 |
| Eccentricity: | 0.0028013 |
| inclination: | 82.9327° |
| perigee height: | 959 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 328.4639° |
| argument of perigee: | 232.7422° |
| revolutions per day: | 13.75515434 |
| mean anomaly at epoch: | 191.3569° |
| orbit number at epoch: | 66879 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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