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 20692U 26156.96273557 +.00000000 +00000-0 +43681-3 0 00001
2 20692 63.2942 240.0339 0873564 84.4895 285.5022 13.64638104 09
| Epoch (UTC): | 05 June 2026 23:06:20 |
| Eccentricity: | 0.0873564 |
| inclination: | 63.2942° |
| perigee height: | 373 km |
| apogee height: | 1665 km |
| right ascension of ascending node: | 240.0339° |
| argument of perigee: | 84.4895° |
| revolutions per day: | 13.64638104 |
| mean anomaly at epoch: | 285.5022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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