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 08585U 26150.62050471 +.00000000 +00000-0 +00000-0 0 00008
2 08585 3.9739 272.2663 0012331 273.0675 167.5321 1.00205226 00
| Epoch (UTC): | 30 May 2026 14:53:31 |
| Eccentricity: | 0.0012331 |
| inclination: | 3.9739° |
| perigee height: | 35753 km |
| apogee height: | 35857 km |
| right ascension of ascending node: | 272.2663° |
| argument of perigee: | 273.0675° |
| revolutions per day: | 1.00205226 |
| mean anomaly at epoch: | 167.5321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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