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 26720U 26144.94335057 +.00000000 +00000-0 +00000-0 0 00003
2 26720 10.6852 47.7041 0002391 220.3083 320.7695 0.99180694 05
| Epoch (UTC): | 24 May 2026 22:38:25 |
| Eccentricity: | 0.0002391 |
| inclination: | 10.6852° |
| perigee height: | 36085 km |
| apogee height: | 36105 km |
| right ascension of ascending node: | 47.7041° |
| argument of perigee: | 220.3083° |
| revolutions per day: | 0.99180694 |
| mean anomaly at epoch: | 320.7695° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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