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 03338U 26053.63918384 +.00000000 +00000-0 +25971-3 0 00005
2 03338 80.6635 174.4969 1130738 175.0559 186.2905 12.23549274 02
| Epoch (UTC): | 22 February 2026 15:20:25 |
| Eccentricity: | 0.1130738 |
| inclination: | 80.6635° |
| perigee height: | 678 km |
| apogee height: | 2477 km |
| right ascension of ascending node: | 174.4969° |
| argument of perigee: | 175.0559° |
| revolutions per day: | 12.23549274 |
| mean anomaly at epoch: | 186.2905° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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