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 00671U 26088.18270059 +.00000000 +00000-0 +15810-3 0 00001
2 00671 89.9712 333.3056 0038843 217.8278 142.0139 13.45213557 02
| Epoch (UTC): | 29 March 2026 04:23:05 |
| Eccentricity: | 0.0038843 |
| inclination: | 89.9712° |
| perigee height: | 1061 km |
| apogee height: | 1119 km |
| right ascension of ascending node: | 333.3056° |
| argument of perigee: | 217.8278° |
| revolutions per day: | 13.45213557 |
| mean anomaly at epoch: | 142.0139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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