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 28382U 26148.21033810 +.00000000 +00000-0 +22540-2 0 00000
2 28382 87.8954 237.1241 6995651 123.7145 322.6772 2.62023379 03
| Epoch (UTC): | 28 May 2026 05:02:53 |
| Eccentricity: | 0.6995651 |
| inclination: | 87.8954° |
| perigee height: | 299 km |
| apogee height: | 31395 km |
| right ascension of ascending node: | 237.1241° |
| argument of perigee: | 123.7145° |
| revolutions per day: | 2.62023379 |
| mean anomaly at epoch: | 322.6772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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