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 26131.92533310 +.00000000 +00000-0 +42806-4 0 00007
2 28380 82.9580 101.6901 0039180 356.0383 16.5064 13.76331536 02
| Epoch (UTC): | 11 May 2026 22:12:28 |
| Eccentricity: | 0.0039180 |
| inclination: | 82.9580° |
| perigee height: | 948 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 101.6901° |
| argument of perigee: | 356.0383° |
| revolutions per day: | 13.76331536 |
| mean anomaly at epoch: | 16.5064° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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