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 26109.26411008 +.00000000 +00000-0 +30483-3 0 00003
2 40014 98.0408 198.4028 0028644 24.7128 335.5468 15.14992077 09
| Epoch (UTC): | 19 April 2026 06:20:19 |
| Eccentricity: | 0.0028644 |
| inclination: | 98.0408° |
| perigee height: | 501 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 198.4028° |
| argument of perigee: | 24.7128° |
| revolutions per day: | 15.14992077 |
| mean anomaly at epoch: | 335.5468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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