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 00167U 26088.19720744 +.00000000 +00000-0 +13193-3 0 00005
2 00167 47.8457 39.8082 0089688 144.3627 216.3289 14.24134210 00
| Epoch (UTC): | 29 March 2026 04:43:58 |
| Eccentricity: | 0.0089688 |
| inclination: | 47.8457° |
| perigee height: | 747 km |
| apogee height: | 876 km |
| right ascension of ascending node: | 39.8082° |
| argument of perigee: | 144.3627° |
| revolutions per day: | 14.24134210 |
| mean anomaly at epoch: | 216.3289° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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