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 26083.59638429 +.00000000 +00000-0 +26661-3 0 00004
2 00020 33.3482 211.5090 1637913 320.0465 29.0158 11.61890010 07
| Epoch (UTC): | 24 March 2026 14:18:47 |
| Eccentricity: | 0.1637913 |
| inclination: | 33.3482° |
| perigee height: | 507 km |
| apogee height: | 3205 km |
| right ascension of ascending node: | 211.5090° |
| argument of perigee: | 320.0465° |
| revolutions per day: | 11.61890010 |
| mean anomaly at epoch: | 29.0158° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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