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 is defined by the following mean orbital elements,
1 45099U 20006BH 25043.78709733 .11584837 12500-4 44533-3 0 9994
2 45099 53.0203 154.5510 0003460 296.6714 205.3999 16.44022240279191
| Epoch (UTC): | 12 February 2025 18:53:25 |
| Eccentricity: | 0.0003460 |
| inclination: | 53.0203° |
| perigee height: | 153 km |
| apogee height: | 157 km |
| right ascension of ascending node: | 154.5510° |
| argument of perigee: | 296.6714° |
| revolutions per day: | 16.44022240 |
| mean anomaly at epoch: | 205.3999° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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