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 40069U 26032.50185044 +.00000000 +00000-0 +13227-3 0 00000
2 40069 98.4958 13.1577 0006908 73.3932 286.8004 14.21412431 09
| Epoch (UTC): | 01 February 2026 12:02:39 |
| Eccentricity: | 0.0006908 |
| inclination: | 98.4958° |
| perigee height: | 816 km |
| apogee height: | 826 km |
| right ascension of ascending node: | 13.1577° |
| argument of perigee: | 73.3932° |
| revolutions per day: | 14.21412431 |
| mean anomaly at epoch: | 286.8004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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