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 10703U 26105.96185036 +.00000000 +00000-0 -10478-3 0 00000
2 10703 99.3271 101.2686 0008526 138.5581 248.3545 13.99783505 01
| Epoch (UTC): | 15 April 2026 23:05:03 |
| Eccentricity: | 0.0008526 |
| inclination: | 99.3271° |
| perigee height: | 888 km |
| apogee height: | 901 km |
| right ascension of ascending node: | 101.2686° |
| argument of perigee: | 138.5581° |
| revolutions per day: | 13.99783505 |
| mean anomaly at epoch: | 248.3545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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