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 62991U 26145.01543663 +.00000000 +00000-0 +12883-2 0 00000
2 62991 42.9969 261.6416 0003388 282.0407 78.0081 15.70907333 01
| Epoch (UTC): | 25 May 2026 00:22:13 |
| Eccentricity: | 0.0003388 |
| inclination: | 42.9969° |
| perigee height: | 354 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 261.6416° |
| argument of perigee: | 282.0407° |
| revolutions per day: | 15.70907333 |
| mean anomaly at epoch: | 78.0081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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