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 45367U 26066.52807325 +.00000000 +00000-0 +13367-2 0 00002
2 45367 53.0531 165.0953 0001643 355.3957 4.7033 15.43851768 09
| Epoch (UTC): | 07 March 2026 12:40:25 |
| Eccentricity: | 0.0001643 |
| inclination: | 53.0531° |
| perigee height: | 434 km |
| apogee height: | 436 km |
| right ascension of ascending node: | 165.0953° |
| argument of perigee: | 355.3957° |
| revolutions per day: | 15.43851768 |
| mean anomaly at epoch: | 4.7033° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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