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 20202U 26145.79392527 +.00000000 +00000-0 +00000-0 0 00001
2 20202 12.9283 336.6723 0017647 274.4682 259.2633 0.98613138 00
| Epoch (UTC): | 25 May 2026 19:03:15 |
| Eccentricity: | 0.0017647 |
| inclination: | 12.9283° |
| perigee height: | 36183 km |
| apogee height: | 36333 km |
| right ascension of ascending node: | 336.6723° |
| argument of perigee: | 274.4682° |
| revolutions per day: | 0.98613138 |
| mean anomaly at epoch: | 259.2633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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