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 26152.52270968 +.00000000 +00000-0 +10493-3 0 00002
2 00671 89.9633 333.0789 0041364 37.7177 322.6858 13.45223288 09
| Epoch (UTC): | 01 June 2026 12:32:42 |
| Eccentricity: | 0.0041364 |
| inclination: | 89.9633° |
| perigee height: | 1059 km |
| apogee height: | 1121 km |
| right ascension of ascending node: | 333.0789° |
| argument of perigee: | 37.7177° |
| revolutions per day: | 13.45223288 |
| mean anomaly at epoch: | 322.6858° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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