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 40053U 26071.33515241 +.00000000 +00000-0 +11808-3 0 00006
2 40053 98.0737 136.2827 0001444 100.1593 259.9771 14.60864849 09
| Epoch (UTC): | 12 March 2026 08:02:37 |
| Eccentricity: | 0.0001444 |
| inclination: | 98.0737° |
| perigee height: | 689 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 136.2827° |
| argument of perigee: | 100.1593° |
| revolutions per day: | 14.60864849 |
| mean anomaly at epoch: | 259.9771° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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