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 26288.66443094 +.00000000 +00000-0 +20528-3 0 00002
2 40012 97.8044 79.4250 0045179 32.6496 327.7499 14.88750569 08
| Epoch (UTC): | 15 October 2026 15:56:46 |
| Eccentricity: | 0.0045179 |
| inclination: | 97.8044° |
| perigee height: | 570 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 79.4250° |
| argument of perigee: | 32.6496° |
| revolutions per day: | 14.88750569 |
| mean anomaly at epoch: | 327.7499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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