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 51726U 26144.94332310 +.00000000 +00000-0 +91006-3 0 00005
2 51726 53.2168 336.3115 0001727 115.9860 244.1312 15.10822683 00
| Epoch (UTC): | 24 May 2026 22:38:23 |
| Eccentricity: | 0.0001727 |
| inclination: | 53.2168° |
| perigee height: | 532 km |
| apogee height: | 535 km |
| right ascension of ascending node: | 336.3115° |
| argument of perigee: | 115.9860° |
| revolutions per day: | 15.10822683 |
| mean anomaly at epoch: | 244.1312° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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