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 40101U 26139.75805608 +.00000000 +00000-0 +00000-0 0 00009
2 40101 9.1736 57.5469 0014203 332.0156 224.7775 0.98724906 09
| Epoch (UTC): | 19 May 2026 18:11:36 |
| Eccentricity: | 0.0014203 |
| inclination: | 9.1736° |
| perigee height: | 36165 km |
| apogee height: | 36286 km |
| right ascension of ascending node: | 57.5469° |
| argument of perigee: | 332.0156° |
| revolutions per day: | 0.98724906 |
| mean anomaly at epoch: | 224.7775° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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