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 26049.20966745 +.00000000 +00000-0 +12511-2 0 00003
2 00053 47.2796 349.3482 0098436 83.3151 277.8830 12.17402559 00
| Epoch (UTC): | 18 February 2026 05:01:55 |
| Eccentricity: | 0.0098436 |
| inclination: | 47.2796° |
| perigee height: | 1525 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 349.3482° |
| argument of perigee: | 83.3151° |
| revolutions per day: | 12.17402559 |
| mean anomaly at epoch: | 277.8830° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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