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 28190U 26144.95289661 +.00000000 +00000-0 +00000-0 0 00006
2 28190 54.8497 276.6255 0115098 172.0582 185.2227 2.00555464 09
| Epoch (UTC): | 24 May 2026 22:52:10 |
| Eccentricity: | 0.0115098 |
| inclination: | 54.8497° |
| perigee height: | 19877 km |
| apogee height: | 20489 km |
| right ascension of ascending node: | 276.6255° |
| argument of perigee: | 172.0582° |
| revolutions per day: | 2.00555464 |
| mean anomaly at epoch: | 185.2227° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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