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 26135.25296709 +.00000000 +00000-0 +12095-3 0 00008
2 00107 28.7767 146.3183 0494078 180.7270 179.2608 14.21990418 02
| Epoch (UTC): | 15 May 2026 06:04:16 |
| Eccentricity: | 0.0494078 |
| inclination: | 28.7767° |
| perigee height: | 463 km |
| apogee height: | 1174 km |
| right ascension of ascending node: | 146.3183° |
| argument of perigee: | 180.7270° |
| revolutions per day: | 14.21990418 |
| mean anomaly at epoch: | 179.2608° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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