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 20625U 90046B 25173.12279112 .00000248 00000-0 15267-3 0 9995
2 20625 70.9983 125.1270 0014942 332.9934 27.0410 14.14964791811789
| Epoch (UTC): | 22 June 2025 02:56:49 |
| Eccentricity: | 0.0014942 |
| inclination: | 70.9983° |
| perigee height: | 831 km |
| apogee height: | 853 km |
| right ascension of ascending node: | 125.1270° |
| argument of perigee: | 332.9934° |
| revolutions per day: | 14.14964791 |
| mean anomaly at epoch: | 27.0410° |
| orbit number at epoch: | 81178 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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