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 40055U 26071.21069546 +.00000000 +00000-0 +18377-3 0 00005
2 40055 98.3273 302.8952 0012187 328.0575 31.9896 14.81069251 09
| Epoch (UTC): | 12 March 2026 05:03:24 |
| Eccentricity: | 0.0012187 |
| inclination: | 98.3273° |
| perigee height: | 617 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 302.8952° |
| argument of perigee: | 328.0575° |
| revolutions per day: | 14.81069251 |
| mean anomaly at epoch: | 31.9896° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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