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 07369U 74054A 25012.28505042 .00000007 00000-0 00000-0 0 9998
2 07369 124.6578 186.6650 0067259 44.5526 126.1981 3.07214420566612
| Epoch (UTC): | 12 January 2025 06:50:28 |
| Eccentricity: | 0.0067259 |
| inclination: | 124.6578° |
| perigee height: | 13475 km |
| apogee height: | 13744 km |
| right ascension of ascending node: | 186.6650° |
| argument of perigee: | 44.5526° |
| revolutions per day: | 3.07214420 |
| mean anomaly at epoch: | 126.1981° |
| orbit number at epoch: | 56661 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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