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 26072.97244502 +.00000000 +00000-0 +19692-3 0 00000
2 20663 62.7915 320.9716 0016418 191.1309 168.9431 15.05678292 08
| Epoch (UTC): | 13 March 2026 23:20:19 |
| Eccentricity: | 0.0016418 |
| inclination: | 62.7915° |
| perigee height: | 538 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 320.9716° |
| argument of perigee: | 191.1309° |
| revolutions per day: | 15.05678292 |
| mean anomaly at epoch: | 168.9431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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