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 26880U 26139.81248300 +.00000000 +00000-0 +00000-0 0 00004
2 26880 12.7563 16.6373 0000604 124.5653 47.1930 0.99200401 01
| Epoch (UTC): | 19 May 2026 19:29:58 |
| Eccentricity: | 0.0000604 |
| inclination: | 12.7563° |
| perigee height: | 36087 km |
| apogee height: | 36092 km |
| right ascension of ascending node: | 16.6373° |
| argument of perigee: | 124.5653° |
| revolutions per day: | 0.99200401 |
| mean anomaly at epoch: | 47.1930° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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