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 40118U 26145.60856793 +.00000000 +00000-0 +14243-3 0 00006
2 40118 98.0116 209.8366 0006275 315.3517 44.7190 14.80872503 03
| Epoch (UTC): | 25 May 2026 14:36:20 |
| Eccentricity: | 0.0006275 |
| inclination: | 98.0116° |
| perigee height: | 622 km |
| apogee height: | 631 km |
| right ascension of ascending node: | 209.8366° |
| argument of perigee: | 315.3517° |
| revolutions per day: | 14.80872503 |
| mean anomaly at epoch: | 44.7190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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