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 16625U 86014F 25198.50403598 .00005046 00000-0 44378-3 0 9992
2 16625 63.2997 296.2786 0817020 109.5973 259.5074 13.70444189296886
| Epoch (UTC): | 17 July 2025 12:05:48 |
| Eccentricity: | 0.0817020 |
| inclination: | 63.2997° |
| perigee height: | 395 km |
| apogee height: | 1600 km |
| right ascension of ascending node: | 296.2786° |
| argument of perigee: | 109.5973° |
| revolutions per day: | 13.70444189 |
| mean anomaly at epoch: | 259.5074° |
| orbit number at epoch: | 29688 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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