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 10120U 26088.18198350 +.00000000 +00000-0 +63487-4 0 00008
2 10120 74.0493 169.2800 0011610 110.6179 249.6218 14.32878487 07
| Epoch (UTC): | 29 March 2026 04:22:03 |
| Eccentricity: | 0.0011610 |
| inclination: | 74.0493° |
| perigee height: | 774 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 169.2800° |
| argument of perigee: | 110.6179° |
| revolutions per day: | 14.32878487 |
| mean anomaly at epoch: | 249.6218° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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