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 19650U 88102B 25188.72706957 .00000228 00000-0 13963-3 0 9994
2 19650 71.0006 306.9008 0013544 15.5089 344.6446 14.16106380892211
| Epoch (UTC): | 07 July 2025 17:26:58 |
| Eccentricity: | 0.0013544 |
| inclination: | 71.0006° |
| perigee height: | 829 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 306.9008° |
| argument of perigee: | 15.5089° |
| revolutions per day: | 14.16106380 |
| mean anomaly at epoch: | 344.6446° |
| orbit number at epoch: | 89221 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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