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 26105.86975062 +.00000000 +00000-0 +11720-3 0 00009
2 31128 98.4343 74.3519 0083746 274.9451 84.2193 14.63646272 05
| Epoch (UTC): | 15 April 2026 20:52:26 |
| Eccentricity: | 0.0083746 |
| inclination: | 98.4343° |
| perigee height: | 622 km |
| apogee height: | 741 km |
| right ascension of ascending node: | 74.3519° |
| argument of perigee: | 274.9451° |
| revolutions per day: | 14.63646272 |
| mean anomaly at epoch: | 84.2193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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