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 66874U 26042.26221222 +.00000000 +00000-0 +10743-2 0 00004
2 66874 42.9905 132.7189 0002201 151.9481 208.1489 15.27588464 09
| Epoch (UTC): | 11 February 2026 06:17:35 |
| Eccentricity: | 0.0002201 |
| inclination: | 42.9905° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 132.7189° |
| argument of perigee: | 151.9481° |
| revolutions per day: | 15.27588464 |
| mean anomaly at epoch: | 208.1489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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