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 26070.49139648 +.00000000 +00000-0 +20180-3 0 00009
2 53807 53.2293 132.2287 0004717 231.4523 128.6060 15.37178618 03
| Epoch (UTC): | 11 March 2026 11:47:36 |
| Eccentricity: | 0.0004717 |
| inclination: | 53.2293° |
| perigee height: | 451 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 132.2287° |
| argument of perigee: | 231.4523° |
| revolutions per day: | 15.37178618 |
| mean anomaly at epoch: | 128.6060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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