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 31118U 26145.61386632 +.00000000 +00000-0 +45657-4 0 00001
2 31118 98.1446 96.0018 0013475 302.5205 57.4699 14.71409515 06
| Epoch (UTC): | 25 May 2026 14:43:58 |
| Eccentricity: | 0.0013475 |
| inclination: | 98.1446° |
| perigee height: | 647 km |
| apogee height: | 666 km |
| right ascension of ascending node: | 96.0018° |
| argument of perigee: | 302.5205° |
| revolutions per day: | 14.71409515 |
| mean anomaly at epoch: | 57.4699° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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