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 28380U 26042.28941181 +.00000000 +00000-0 +73253-4 0 00006
2 28380 82.9638 168.0643 0038105 243.3930 133.8760 13.76321935 06
| Epoch (UTC): | 11 February 2026 06:56:45 |
| Eccentricity: | 0.0038105 |
| inclination: | 82.9638° |
| perigee height: | 949 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 168.0643° |
| argument of perigee: | 243.3930° |
| revolutions per day: | 13.76321935 |
| mean anomaly at epoch: | 133.8760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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