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 21228U 91028B 25198.50320130 .00000242 00000-0 44122-4 0 9999
2 21228 23.9882 234.9759 1134881 96.5206 276.5440 12.55277916568352
| Epoch (UTC): | 17 July 2025 12:04:36 |
| Eccentricity: | 0.1134881 |
| inclination: | 23.9882° |
| perigee height: | 555 km |
| apogee height: | 2330 km |
| right ascension of ascending node: | 234.9759° |
| argument of perigee: | 96.5206° |
| revolutions per day: | 12.55277916 |
| mean anomaly at epoch: | 276.5440° |
| orbit number at epoch: | 56835 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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