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 01430U 26070.94266037 +.00000000 +00000-0 +72251-4 0 00004
2 01430 98.4889 190.7738 0055454 12.2336 348.0185 14.41589810 01
| Epoch (UTC): | 11 March 2026 22:37:25 |
| Eccentricity: | 0.0055454 |
| inclination: | 98.4889° |
| perigee height: | 714 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 190.7738° |
| argument of perigee: | 12.2336° |
| revolutions per day: | 14.41589810 |
| mean anomaly at epoch: | 348.0185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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