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 53807U 26138.35382905 +.00000000 +00000-0 +94066-4 0 00000
2 53807 53.2275 173.9872 0007418 82.5786 277.6061 15.37873814 08
| Epoch (UTC): | 18 May 2026 08:29:30 |
| Eccentricity: | 0.0007418 |
| inclination: | 53.2275° |
| perigee height: | 447 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 173.9872° |
| argument of perigee: | 82.5786° |
| revolutions per day: | 15.37873814 |
| mean anomaly at epoch: | 277.6061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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