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 26106.57998741 +.00000000 +00000-0 +35071-4 0 00002
2 31118 98.1408 56.9607 0015921 65.7298 294.5570 14.71386556 02
| Epoch (UTC): | 16 April 2026 13:55:10 |
| Eccentricity: | 0.0015921 |
| inclination: | 98.1408° |
| perigee height: | 645 km |
| apogee height: | 668 km |
| right ascension of ascending node: | 56.9607° |
| argument of perigee: | 65.7298° |
| revolutions per day: | 14.71386556 |
| mean anomaly at epoch: | 294.5570° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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