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 26068.41722530 +.00000000 +00000-0 +86155-3 0 00008
2 40368 24.6888 75.6595 7270441 179.2102 183.5993 2.26120442 04
| Epoch (UTC): | 09 March 2026 10:00:48 |
| Eccentricity: | 0.7270441 |
| inclination: | 24.6888° |
| perigee height: | 315 km |
| apogee height: | 35968 km |
| right ascension of ascending node: | 75.6595° |
| argument of perigee: | 179.2102° |
| revolutions per day: | 2.26120442 |
| mean anomaly at epoch: | 183.5993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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