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 53609U 26145.55681095 +.00000000 +00000-0 +58446-4 0 00004
2 53609 53.2111 253.7482 0001097 87.5378 272.5740 15.08838535 07
| Epoch (UTC): | 25 May 2026 13:21:48 |
| Eccentricity: | 0.0001097 |
| inclination: | 53.2111° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 253.7482° |
| argument of perigee: | 87.5378° |
| revolutions per day: | 15.08838535 |
| mean anomaly at epoch: | 272.5740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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