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 26071.43113030 +.00000000 +00000-0 +43692-3 0 00008
2 40012 97.7730 225.9555 0045882 28.9236 331.4508 14.87659811 06
| Epoch (UTC): | 12 March 2026 10:20:49 |
| Eccentricity: | 0.0045882 |
| inclination: | 97.7730° |
| perigee height: | 573 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 225.9555° |
| argument of perigee: | 28.9236° |
| revolutions per day: | 14.87659811 |
| mean anomaly at epoch: | 331.4508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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