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 26137.83392079 +.00000000 +00000-0 +11478-3 0 00000
2 53807 53.2277 176.4267 0007407 81.3185 278.8658 15.37870657 01
| Epoch (UTC): | 17 May 2026 20:00:50 |
| Eccentricity: | 0.0007407 |
| inclination: | 53.2277° |
| perigee height: | 447 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 176.4267° |
| argument of perigee: | 81.3185° |
| revolutions per day: | 15.37870657 |
| mean anomaly at epoch: | 278.8658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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