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 26104.20711797 +.00000000 +00000-0 -27487-3 0 00000
2 00053 47.2769 179.6951 0100880 246.1666 112.8522 12.17408908 02
| Epoch (UTC): | 14 April 2026 04:58:14 |
| Eccentricity: | 0.0100880 |
| inclination: | 47.2769° |
| perigee height: | 1523 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 179.6951° |
| argument of perigee: | 246.1666° |
| revolutions per day: | 12.17408908 |
| mean anomaly at epoch: | 112.8522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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