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 31789U 07028A 25196.80229416 .00121407 12116-4 47475-3 0 9990
2 31789 64.4715 286.9022 0026074 303.5588 56.3078 15.86422594998648
| Epoch (UTC): | 15 July 2025 19:15:18 |
| Eccentricity: | 0.0026074 |
| inclination: | 64.4715° |
| perigee height: | 295 km |
| apogee height: | 330 km |
| right ascension of ascending node: | 286.9022° |
| argument of perigee: | 303.5588° |
| revolutions per day: | 15.86422594 |
| mean anomaly at epoch: | 56.3078° |
| orbit number at epoch: | 99864 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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