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 26074.25417299 +.00000000 +00000-0 +48613-3 0 00005
2 40014 98.0425 161.3943 0029535 140.1254 220.2154 15.14583059 04
| Epoch (UTC): | 15 March 2026 06:06:00 |
| Eccentricity: | 0.0029535 |
| inclination: | 98.0425° |
| perigee height: | 502 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 161.3943° |
| argument of perigee: | 140.1254° |
| revolutions per day: | 15.14583059 |
| mean anomaly at epoch: | 220.2154° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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