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 26069.95041984 +.00000000 +00000-0 -90441-5 0 00009
2 40069 98.5035 49.2166 0005264 333.9413 26.1499 14.21428814 08
| Epoch (UTC): | 10 March 2026 22:48:36 |
| Eccentricity: | 0.0005264 |
| inclination: | 98.5035° |
| perigee height: | 817 km |
| apogee height: | 824 km |
| right ascension of ascending node: | 49.2166° |
| argument of perigee: | 333.9413° |
| revolutions per day: | 14.21428814 |
| mean anomaly at epoch: | 26.1499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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