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 35951U 26140.56170103 +.00000000 +00000-0 +12170-3 0 00006
2 35951 98.9028 121.3933 0010591 335.7240 24.3432 14.14879750 07
| Epoch (UTC): | 20 May 2026 13:28:50 |
| Eccentricity: | 0.0010591 |
| inclination: | 98.9028° |
| perigee height: | 835 km |
| apogee height: | 850 km |
| right ascension of ascending node: | 121.3933° |
| argument of perigee: | 335.7240° |
| revolutions per day: | 14.14879750 |
| mean anomaly at epoch: | 24.3432° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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