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 62990U 26145.36599176 +.00000000 +00000-0 +17181-2 0 00003
2 62990 43.0030 259.0932 0005283 282.3462 77.6814 15.70839815 03
| Epoch (UTC): | 25 May 2026 08:47:01 |
| Eccentricity: | 0.0005283 |
| inclination: | 43.0030° |
| perigee height: | 353 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 259.0932° |
| argument of perigee: | 282.3462° |
| revolutions per day: | 15.70839815 |
| mean anomaly at epoch: | 77.6814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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