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 00045U 60007A 25173.44389289 .00000120 00000-0 56340-4 0 9992
2 00045 66.6927 231.4732 0242996 60.8855 301.6336 14.35560955328405
| Epoch (UTC): | 22 June 2025 10:39:12 |
| Eccentricity: | 0.0242996 |
| inclination: | 66.6927° |
| perigee height: | 599 km |
| apogee height: | 947 km |
| right ascension of ascending node: | 231.4732° |
| argument of perigee: | 60.8855° |
| revolutions per day: | 14.35560955 |
| mean anomaly at epoch: | 301.6336° |
| orbit number at epoch: | 32840 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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