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 31121U 26145.37683323 +.00000000 +00000-0 +12630-3 0 00009
2 31121 98.4084 112.4720 0072686 38.6808 321.9567 14.62522381 09
| Epoch (UTC): | 25 May 2026 09:02:38 |
| Eccentricity: | 0.0072686 |
| inclination: | 98.4084° |
| perigee height: | 634 km |
| apogee height: | 736 km |
| right ascension of ascending node: | 112.4720° |
| argument of perigee: | 38.6808° |
| revolutions per day: | 14.62522381 |
| mean anomaly at epoch: | 321.9567° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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