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 34713U 26052.93475545 +.00000000 +00000-0 +00000-0 0 00008
2 34713 0.0227 120.8304 0000834 215.3922 209.6545 1.00271650 01
| Epoch (UTC): | 21 February 2026 22:26:02 |
| Eccentricity: | 0.0000834 |
| inclination: | 0.0227° |
| perigee height: | 35783 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 120.8304° |
| argument of perigee: | 215.3922° |
| revolutions per day: | 1.00271650 |
| mean anomaly at epoch: | 209.6545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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