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 25347.67372262 .00000509 00000-0 14720-3 0 9999
2 00045 66.6925 130.8639 0255677 293.9417 63.5097 14.35782765353416
| Epoch (UTC): | 13 December 2025 16:10:09 |
| Eccentricity: | 0.0255677 |
| inclination: | 66.6925° |
| perigee height: | 589 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 130.8639° |
| argument of perigee: | 293.9417° |
| revolutions per day: | 14.35782765 |
| mean anomaly at epoch: | 63.5097° |
| orbit number at epoch: | 35341 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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