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 28381U 26044.71966454 +.00000000 +00000-0 +47385-4 0 00004
2 28381 82.9605 143.1614 0032758 146.9449 323.1851 13.78607823 04
| Epoch (UTC): | 13 February 2026 17:16:19 |
| Eccentricity: | 0.0032758 |
| inclination: | 82.9605° |
| perigee height: | 945 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 143.1614° |
| argument of perigee: | 146.9449° |
| revolutions per day: | 13.78607823 |
| mean anomaly at epoch: | 323.1851° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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