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 07210U 74011B 25197.94748361 .00000147 00000-0 69624-4 0 9992
2 07210 81.2349 36.7550 0079392 262.1463 97.0692 14.13558900646622
| Epoch (UTC): | 16 July 2025 22:44:22 |
| Eccentricity: | 0.0079392 |
| inclination: | 81.2349° |
| perigee height: | 790 km |
| apogee height: | 904 km |
| right ascension of ascending node: | 36.7550° |
| argument of perigee: | 262.1463° |
| revolutions per day: | 14.13558900 |
| mean anomaly at epoch: | 97.0692° |
| orbit number at epoch: | 64662 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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