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 26074.92865447 +.00000000 +00000-0 +27742-3 0 00009
2 40012 97.7731 229.3833 0045632 17.5226 342.7553 14.87684707 07
| Epoch (UTC): | 15 March 2026 22:17:15 |
| Eccentricity: | 0.0045632 |
| inclination: | 97.7731° |
| perigee height: | 573 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 229.3833° |
| argument of perigee: | 17.5226° |
| revolutions per day: | 14.87684707 |
| mean anomaly at epoch: | 342.7553° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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