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 20641U 26137.31218164 +.00000000 +00000-0 +00000-0 0 00001
2 20641 63.3920 100.1831 4060671 266.2770 47.7615 6.02596074 05
| Epoch (UTC): | 17 May 2026 07:29:32 |
| Eccentricity: | 0.4060671 |
| inclination: | 63.3920° |
| perigee height: | 1198 km |
| apogee height: | 11558 km |
| right ascension of ascending node: | 100.1831° |
| argument of perigee: | 266.2770° |
| revolutions per day: | 6.02596074 |
| mean anomaly at epoch: | 47.7615° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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