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 53145U 26145.53890543 +.00000000 +00000-0 -10299-4 0 00002
2 53145 53.2107 189.1311 0000801 71.1136 288.9943 15.08839571 00
| Epoch (UTC): | 25 May 2026 12:56:01 |
| Eccentricity: | 0.0000801 |
| inclination: | 53.2107° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 189.1311° |
| argument of perigee: | 71.1136° |
| revolutions per day: | 15.08839571 |
| mean anomaly at epoch: | 288.9943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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