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 10674U 26053.59862171 +.00000000 +00000-0 +48624-4 0 00004
2 10674 69.3628 122.3233 0166597 229.5824 240.7714 13.43710374 04
| Epoch (UTC): | 22 February 2026 14:22:00 |
| Eccentricity: | 0.0166597 |
| inclination: | 69.3628° |
| perigee height: | 971 km |
| apogee height: | 1220 km |
| right ascension of ascending node: | 122.3233° |
| argument of perigee: | 229.5824° |
| revolutions per day: | 13.43710374 |
| mean anomaly at epoch: | 240.7714° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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