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 01292U 26088.22217338 +.00000000 +00000-0 +12455-3 0 00009
2 01292 70.0751 123.5691 0017106 50.2035 310.0577 14.01560506 04
| Epoch (UTC): | 29 March 2026 05:19:55 |
| Eccentricity: | 0.0017106 |
| inclination: | 70.0751° |
| perigee height: | 876 km |
| apogee height: | 901 km |
| right ascension of ascending node: | 123.5691° |
| argument of perigee: | 50.2035° |
| revolutions per day: | 14.01560506 |
| mean anomaly at epoch: | 310.0577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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