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 31128U 26102.17815308 +.00000000 +00000-0 +18907-3 0 00000
2 31128 98.4335 70.5745 0083784 286.6332 72.5682 14.63641218 03
| Epoch (UTC): | 12 April 2026 04:16:32 |
| Eccentricity: | 0.0083784 |
| inclination: | 98.4335° |
| perigee height: | 622 km |
| apogee height: | 741 km |
| right ascension of ascending node: | 70.5745° |
| argument of perigee: | 286.6332° |
| revolutions per day: | 14.63641218 |
| mean anomaly at epoch: | 72.5682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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