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 53934U 26145.19069723 +.00000000 +00000-0 +40847-4 0 00009
2 53934 53.2136 315.7424 0001260 87.9346 272.1791 15.08835429 02
| Epoch (UTC): | 25 May 2026 04:34:36 |
| Eccentricity: | 0.0001260 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 315.7424° |
| argument of perigee: | 87.9346° |
| revolutions per day: | 15.08835429 |
| mean anomaly at epoch: | 272.1791° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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