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 26145.52055897 +.00000000 +00000-0 +24880-3 0 00006
2 40014 98.0415 236.7498 0026872 257.5655 102.2568 15.15304995 03
| Epoch (UTC): | 25 May 2026 12:29:36 |
| Eccentricity: | 0.0026872 |
| inclination: | 98.0415° |
| perigee height: | 502 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 236.7498° |
| argument of perigee: | 257.5655° |
| revolutions per day: | 15.15304995 |
| mean anomaly at epoch: | 102.2568° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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