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 26131.04283329 +.00000000 +00000-0 +10670-3 0 00006
2 00020 33.3515 40.6601 1637841 214.4801 133.8000 11.61945858 04
| Epoch (UTC): | 11 May 2026 01:01:40 |
| Eccentricity: | 0.1637841 |
| inclination: | 33.3515° |
| perigee height: | 507 km |
| apogee height: | 3204 km |
| right ascension of ascending node: | 40.6601° |
| argument of perigee: | 214.4801° |
| revolutions per day: | 11.61945858 |
| mean anomaly at epoch: | 133.8000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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