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 26037.99926130 +.00000000 +00000-0 +57622-3 0 00002
2 40012 97.7674 193.2148 0046528 136.6885 223.8004 14.87381634 03
| Epoch (UTC): | 06 February 2026 23:58:56 |
| Eccentricity: | 0.0046528 |
| inclination: | 97.7674° |
| perigee height: | 574 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 193.2148° |
| argument of perigee: | 136.6885° |
| revolutions per day: | 14.87381634 |
| mean anomaly at epoch: | 223.8004° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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