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 31130U 26105.87190691 +.00000000 +00000-0 +12293-3 0 00006
2 31130 98.4423 78.7208 0082287 265.7310 93.4485 14.64735950 00
| Epoch (UTC): | 15 April 2026 20:55:32 |
| Eccentricity: | 0.0082287 |
| inclination: | 98.4423° |
| perigee height: | 620 km |
| apogee height: | 736 km |
| right ascension of ascending node: | 78.7208° |
| argument of perigee: | 265.7310° |
| revolutions per day: | 14.64735950 |
| mean anomaly at epoch: | 93.4485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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