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 21667U 91059B 25196.86818093 .00000007 00000-0 -80268-5 0 9999
2 21667 82.9076 331.6255 0019649 310.6678 161.5202 13.75254454700959
| Epoch (UTC): | 15 July 2025 20:50:10 |
| Eccentricity: | 0.0019649 |
| inclination: | 82.9076° |
| perigee height: | 966 km |
| apogee height: | 995 km |
| right ascension of ascending node: | 331.6255° |
| argument of perigee: | 310.6678° |
| revolutions per day: | 13.75254454 |
| mean anomaly at epoch: | 161.5202° |
| orbit number at epoch: | 70095 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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