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 53912U 26145.22054787 +.00000000 +00000-0 +74876-4 0 00002
2 53912 53.2144 330.2010 0001322 88.3888 271.7255 15.08832104 02
| Epoch (UTC): | 25 May 2026 05:17:35 |
| Eccentricity: | 0.0001322 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 330.2010° |
| argument of perigee: | 88.3888° |
| revolutions per day: | 15.08832104 |
| mean anomaly at epoch: | 271.7255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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