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 49336U 26144.68224374 +.00000000 +00000-0 +00000-0 0 00001
2 49336 37.4165 79.9290 0753260 271.3756 271.7509 1.00263785 06
| Epoch (UTC): | 24 May 2026 16:22:25 |
| Eccentricity: | 0.0753260 |
| inclination: | 37.4165° |
| perigee height: | 32613 km |
| apogee height: | 38965 km |
| right ascension of ascending node: | 79.9290° |
| argument of perigee: | 271.3756° |
| revolutions per day: | 1.00263785 |
| mean anomaly at epoch: | 271.7509° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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