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 26156.67986977 +.00000000 +00000-0 +25013-3 0 00005
2 40014 98.0419 248.5570 0027163 218.1640 141.7668 15.15453515 02
| Epoch (UTC): | 05 June 2026 16:19:00 |
| Eccentricity: | 0.0027163 |
| inclination: | 98.0419° |
| perigee height: | 501 km |
| apogee height: | 538 km |
| right ascension of ascending node: | 248.5570° |
| argument of perigee: | 218.1640° |
| revolutions per day: | 15.15453515 |
| mean anomaly at epoch: | 141.7668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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