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 00053U 26129.90018231 +.00000000 +00000-0 +77048-3 0 00004
2 00053 47.2763 100.4362 0101211 322.2220 37.1496 12.17411115 08
| Epoch (UTC): | 09 May 2026 21:36:15 |
| Eccentricity: | 0.0101211 |
| inclination: | 47.2763° |
| perigee height: | 1523 km |
| apogee height: | 1685 km |
| right ascension of ascending node: | 100.4362° |
| argument of perigee: | 322.2220° |
| revolutions per day: | 12.17411115 |
| mean anomaly at epoch: | 37.1496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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