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 26046.91123229 +.00000000 +00000-0 +96674-3 0 00003
2 00053 47.2796 356.4378 0098309 76.5193 284.6529 12.17401794 03
| Epoch (UTC): | 15 February 2026 21:52:10 |
| Eccentricity: | 0.0098309 |
| inclination: | 47.2796° |
| perigee height: | 1525 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 356.4378° |
| argument of perigee: | 76.5193° |
| revolutions per day: | 12.17401794 |
| mean anomaly at epoch: | 284.6529° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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