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 20663U 26074.63277017 +.00000000 +00000-0 +15746-3 0 00008
2 20663 62.7912 315.3087 0016142 191.5948 168.4783 15.05686621 01
| Epoch (UTC): | 15 March 2026 15:11:11 |
| Eccentricity: | 0.0016142 |
| inclination: | 62.7912° |
| perigee height: | 538 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 315.3087° |
| argument of perigee: | 191.5948° |
| revolutions per day: | 15.05686621 |
| mean anomaly at epoch: | 168.4783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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