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 40296U 26032.58358531 +.00000000 +00000-0 +00000-0 0 00005
2 40296 63.4549 228.8459 6703147 271.4179 18.8414 2.00588125 08
| Epoch (UTC): | 01 February 2026 14:00:21 |
| Eccentricity: | 0.6703147 |
| inclination: | 63.4549° |
| perigee height: | 2378 km |
| apogee height: | 37982 km |
| right ascension of ascending node: | 228.8459° |
| argument of perigee: | 271.4179° |
| revolutions per day: | 2.00588125 |
| mean anomaly at epoch: | 18.8414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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