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 62208U 26145.20362691 +.00000000 +00000-0 +52884-3 0 00008
2 62208 43.0007 198.5659 0001565 270.2485 89.8187 15.27606386 07
| Epoch (UTC): | 25 May 2026 04:53:13 |
| Eccentricity: | 0.0001565 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 198.5659° |
| argument of perigee: | 270.2485° |
| revolutions per day: | 15.27606386 |
| mean anomaly at epoch: | 89.8187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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