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 26073.89743097 +.00000000 +00000-0 +40916-3 0 00009
2 00107 28.7764 139.9719 0494380 327.8499 29.2812 14.21779638 05
| Epoch (UTC): | 14 March 2026 21:32:18 |
| Eccentricity: | 0.0494380 |
| inclination: | 28.7764° |
| perigee height: | 464 km |
| apogee height: | 1175 km |
| right ascension of ascending node: | 139.9719° |
| argument of perigee: | 327.8499° |
| revolutions per day: | 14.21779638 |
| mean anomaly at epoch: | 29.2812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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