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 40014U 26049.87274269 +.00000000 +00000-0 +24817-3 0 00003
2 40014 98.0462 135.6280 0028037 222.7842 137.1206 15.14232429 05
| Epoch (UTC): | 18 February 2026 20:56:44 |
| Eccentricity: | 0.0028037 |
| inclination: | 98.0462° |
| perigee height: | 504 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 135.6280° |
| argument of perigee: | 222.7842° |
| revolutions per day: | 15.14232429 |
| mean anomaly at epoch: | 137.1206° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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