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 62983U 26145.34397325 +.00000000 +00000-0 +22022-2 0 00005
2 62983 42.9990 259.8148 0001941 276.7709 83.2938 15.70924359 01
| Epoch (UTC): | 25 May 2026 08:15:19 |
| Eccentricity: | 0.0001941 |
| inclination: | 42.9990° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 259.8148° |
| argument of perigee: | 276.7709° |
| revolutions per day: | 15.70924359 |
| mean anomaly at epoch: | 83.2938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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