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 53992U 26145.53524353 +.00000000 +00000-0 +63171-4 0 00001
2 53992 53.2114 229.1463 0001352 66.9708 293.1427 15.08834567 05
| Epoch (UTC): | 25 May 2026 12:50:45 |
| Eccentricity: | 0.0001352 |
| inclination: | 53.2114° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 229.1463° |
| argument of perigee: | 66.9708° |
| revolutions per day: | 15.08834567 |
| mean anomaly at epoch: | 293.1427° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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