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 20929U 26140.40524795 +.00000000 +00000-0 +00000-0 0 00004
2 20929 14.0211 344.2427 0004214 75.3968 95.5646 0.98398033 06
| Epoch (UTC): | 20 May 2026 09:43:33 |
| Eccentricity: | 0.0004214 |
| inclination: | 14.0211° |
| perigee height: | 36302 km |
| apogee height: | 36338 km |
| right ascension of ascending node: | 344.2427° |
| argument of perigee: | 75.3968° |
| revolutions per day: | 0.98398033 |
| mean anomaly at epoch: | 95.5646° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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