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 26040.28159000 +.00000000 +00000-0 +65211-4 0 00001
2 28381 82.9606 146.4604 0032447 159.1711 257.3129 13.78607267 01
| Epoch (UTC): | 09 February 2026 06:45:29 |
| Eccentricity: | 0.0032447 |
| inclination: | 82.9606° |
| perigee height: | 945 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 146.4604° |
| argument of perigee: | 159.1711° |
| revolutions per day: | 13.78607267 |
| mean anomaly at epoch: | 257.3129° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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