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 26075.24516382 +.00000000 +00000-0 +38853-3 0 00003
2 40014 98.0429 162.4418 0029546 136.7434 223.6124 15.14595839 03
| Epoch (UTC): | 16 March 2026 05:53:02 |
| Eccentricity: | 0.0029546 |
| inclination: | 98.0429° |
| perigee height: | 502 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 162.4418° |
| argument of perigee: | 136.7434° |
| revolutions per day: | 15.14595839 |
| mean anomaly at epoch: | 223.6124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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