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 25073.53441767 .00000781 00000-0 21939-3 0 9999
2 00045 66.6930 135.5097 0244848 135.9352 226.1554 14.35420477314065
| Epoch (UTC): | 14 March 2025 12:49:33 |
| Eccentricity: | 0.0244848 |
| inclination: | 66.6930° |
| perigee height: | 598 km |
| apogee height: | 949 km |
| right ascension of ascending node: | 135.5097° |
| argument of perigee: | 135.9352° |
| revolutions per day: | 14.35420477 |
| mean anomaly at epoch: | 226.1554° |
| orbit number at epoch: | 31406 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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