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 00020U 26038.04477968 +.00000000 +00000-0 +53654-3 0 00005
2 00020 33.3448 15.4858 1638325 75.8862 301.7698 11.61807632 03
| Epoch (UTC): | 07 February 2026 01:04:28 |
| Eccentricity: | 0.1638325 |
| inclination: | 33.3448° |
| perigee height: | 507 km |
| apogee height: | 3206 km |
| right ascension of ascending node: | 15.4858° |
| argument of perigee: | 75.8862° |
| revolutions per day: | 11.61807632 |
| mean anomaly at epoch: | 301.7698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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