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 53892U 26145.51037588 +.00000000 +00000-0 +86356-4 0 00007
2 53892 53.2124 339.1368 0001720 114.3489 245.7683 15.08833018 01
| Epoch (UTC): | 25 May 2026 12:14:56 |
| Eccentricity: | 0.0001720 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 339.1368° |
| argument of perigee: | 114.3489° |
| revolutions per day: | 15.08833018 |
| mean anomaly at epoch: | 245.7683° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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