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 28361U 26144.36519809 +.00000000 +00000-0 +00000-0 0 00001
2 28361 54.8487 87.6732 0160271 301.2714 171.8878 2.00555817 09
| Epoch (UTC): | 24 May 2026 08:45:53 |
| Eccentricity: | 0.0160271 |
| inclination: | 54.8487° |
| perigee height: | 19757 km |
| apogee height: | 20609 km |
| right ascension of ascending node: | 87.6732° |
| argument of perigee: | 301.2714° |
| revolutions per day: | 2.00555817 |
| mean anomaly at epoch: | 171.8878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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