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 40368U 26074.14713229 +.00000000 +00000-0 +64446-3 0 00009
2 40368 24.7133 73.5703 7270003 182.8020 168.0416 2.26130839 08
| Epoch (UTC): | 15 March 2026 03:31:52 |
| Eccentricity: | 0.7270003 |
| inclination: | 24.7133° |
| perigee height: | 315 km |
| apogee height: | 35965 km |
| right ascension of ascending node: | 73.5703° |
| argument of perigee: | 182.8020° |
| revolutions per day: | 2.26130839 |
| mean anomaly at epoch: | 168.0416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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