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 00107U 26131.18229810 +.00000000 +00000-0 +13303-3 0 00008
2 00107 28.7752 169.7864 0494166 142.7272 220.8670 14.21982383 03
| Epoch (UTC): | 11 May 2026 04:22:30 |
| Eccentricity: | 0.0494166 |
| inclination: | 28.7752° |
| perigee height: | 463 km |
| apogee height: | 1174 km |
| right ascension of ascending node: | 169.7864° |
| argument of perigee: | 142.7272° |
| revolutions per day: | 14.21982383 |
| mean anomaly at epoch: | 220.8670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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