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 53616U 26145.52325392 +.00000000 +00000-0 +22319-3 0 00003
2 53616 53.2148 239.0748 0000997 88.1255 271.9852 15.08829109 00
| Epoch (UTC): | 25 May 2026 12:33:29 |
| Eccentricity: | 0.0000997 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 239.0748° |
| argument of perigee: | 88.1255° |
| revolutions per day: | 15.08829109 |
| mean anomaly at epoch: | 271.9852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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