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 52673U 26145.47450315 +.00000000 +00000-0 +17633-4 0 00007
2 52673 53.2136 169.4177 0001158 107.7087 252.4032 15.08843242 00
| Epoch (UTC): | 25 May 2026 11:23:17 |
| Eccentricity: | 0.0001158 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 169.4177° |
| argument of perigee: | 107.7087° |
| revolutions per day: | 15.08843242 |
| mean anomaly at epoch: | 252.4032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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