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 28912U 26144.87980756 +.00000000 +00000-0 +00000-0 0 00002
2 28912 9.3116 54.3974 0001505 324.0196 226.4452 1.00274292 04
| Epoch (UTC): | 24 May 2026 21:06:55 |
| Eccentricity: | 0.0001505 |
| inclination: | 9.3116° |
| perigee height: | 35780 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 54.3974° |
| argument of perigee: | 324.0196° |
| revolutions per day: | 1.00274292 |
| mean anomaly at epoch: | 226.4452° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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