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 26132.37479839 +.00000000 +00000-0 +84119-4 0 00007
2 53807 53.2287 202.0389 0007381 68.6172 291.5620 15.37834262 01
| Epoch (UTC): | 12 May 2026 08:59:42 |
| Eccentricity: | 0.0007381 |
| inclination: | 53.2287° |
| perigee height: | 447 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 202.0389° |
| argument of perigee: | 68.6172° |
| revolutions per day: | 15.37834262 |
| mean anomaly at epoch: | 291.5620° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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