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 53175U 26145.52788502 +.00000000 +00000-0 +30416-3 0 00006
2 53175 53.2111 189.1797 0001339 85.4877 274.6268 15.08814327 07
| Epoch (UTC): | 25 May 2026 12:40:09 |
| Eccentricity: | 0.0001339 |
| inclination: | 53.2111° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 189.1797° |
| argument of perigee: | 85.4877° |
| revolutions per day: | 15.08814327 |
| mean anomaly at epoch: | 274.6268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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