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 36744U 26144.75354350 +.00000000 +00000-0 +00000-0 0 00006
2 36744 4.7506 75.6577 0001011 328.9933 237.1042 1.00271668 05
| Epoch (UTC): | 24 May 2026 18:05:06 |
| Eccentricity: | 0.0001011 |
| inclination: | 4.7506° |
| perigee height: | 35782 km |
| apogee height: | 35791 km |
| right ascension of ascending node: | 75.6577° |
| argument of perigee: | 328.9933° |
| revolutions per day: | 1.00271668 |
| mean anomaly at epoch: | 237.1042° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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