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 26041.87386751 +.00000000 +00000-0 +73638-4 0 00003
2 28380 82.9637 168.3718 0038093 244.5984 234.9112 13.76321863 03
| Epoch (UTC): | 10 February 2026 20:58:22 |
| Eccentricity: | 0.0038093 |
| inclination: | 82.9637° |
| perigee height: | 949 km |
| apogee height: | 1005 km |
| right ascension of ascending node: | 168.3718° |
| argument of perigee: | 244.5984° |
| revolutions per day: | 13.76321863 |
| mean anomaly at epoch: | 234.9112° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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