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 39222U 13041A 25133.92420104 .00000106 00000-0 00000-0 0 9990
2 39222 0.0183 308.8507 0000088 226.8094 253.7857 1.00271062 42057
| Epoch (UTC): | 13 May 2025 22:10:50 |
| Eccentricity: | 0.0000088 |
| inclination: | 0.0183° |
| perigee height: | 35786 km |
| apogee height: | 35787 km |
| right ascension of ascending node: | 308.8507° |
| argument of perigee: | 226.8094° |
| revolutions per day: | 1.00271062 |
| mean anomaly at epoch: | 253.7857° |
| orbit number at epoch: | 4205 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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