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 26145.37243777 +.00000000 +00000-0 +16108-3 0 00003
2 53807 53.2278 141.0545 0007402 99.4580 260.7262 15.37947146 02
| Epoch (UTC): | 25 May 2026 08:56:18 |
| Eccentricity: | 0.0007402 |
| inclination: | 53.2278° |
| perigee height: | 447 km |
| apogee height: | 457 km |
| right ascension of ascending node: | 141.0545° |
| argument of perigee: | 99.4580° |
| revolutions per day: | 15.37947146 |
| mean anomaly at epoch: | 260.7262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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