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 40012U 26102.83968213 +.00000000 +00000-0 +23317-3 0 00000
2 40012 97.7789 256.7496 0043953 284.1391 75.4944 14.87871547 02
| Epoch (UTC): | 12 April 2026 20:09:08 |
| Eccentricity: | 0.0043953 |
| inclination: | 97.7789° |
| perigee height: | 574 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 256.7496° |
| argument of perigee: | 284.1391° |
| revolutions per day: | 14.87871547 |
| mean anomaly at epoch: | 75.4944° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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