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 53147U 26145.60159865 +.00000000 +00000-0 -12803-2 0 00008
2 53147 53.2098 188.8499 0001258 85.4495 274.6641 15.08682422 05
| Epoch (UTC): | 25 May 2026 14:26:18 |
| Eccentricity: | 0.0001258 |
| inclination: | 53.2098° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 188.8499° |
| argument of perigee: | 85.4495° |
| revolutions per day: | 15.08682422 |
| mean anomaly at epoch: | 274.6641° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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