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 26133.36279888 +.00000000 +00000-0 +89560-4 0 00003
2 00020 33.3536 32.3084 1638008 226.9163 118.2370 11.61947156 05
| Epoch (UTC): | 13 May 2026 08:42:25 |
| Eccentricity: | 0.1638008 |
| inclination: | 33.3536° |
| perigee height: | 507 km |
| apogee height: | 3205 km |
| right ascension of ascending node: | 32.3084° |
| argument of perigee: | 226.9163° |
| revolutions per day: | 11.61947156 |
| mean anomaly at epoch: | 118.2370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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