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 40114U 26105.44460995 +.00000000 +00000-0 +43430-4 0 00006
2 40114 63.3803 208.5628 0385238 14.7475 346.4421 13.44450015 04
| Epoch (UTC): | 15 April 2026 10:40:14 |
| Eccentricity: | 0.0385238 |
| inclination: | 63.3803° |
| perigee height: | 805 km |
| apogee height: | 1381 km |
| right ascension of ascending node: | 208.5628° |
| argument of perigee: | 14.7475° |
| revolutions per day: | 13.44450015 |
| mean anomaly at epoch: | 346.4421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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