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 20763U 26106.89410168 +.00000000 +00000-0 +13404-3 0 00008
2 20763 24.7610 323.4743 0329574 228.6493 128.5218 14.63554640 05
| Epoch (UTC): | 16 April 2026 21:27:30 |
| Eccentricity: | 0.0329574 |
| inclination: | 24.7610° |
| perigee height: | 449 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 323.4743° |
| argument of perigee: | 228.6493° |
| revolutions per day: | 14.63554640 |
| mean anomaly at epoch: | 128.5218° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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