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 40044U 26156.36921817 +.00000000 +00000-0 +31518-3 0 00003
2 40044 97.7870 306.4384 0049647 116.3277 244.3049 14.85195828 04
| Epoch (UTC): | 05 June 2026 08:51:40 |
| Eccentricity: | 0.0049647 |
| inclination: | 97.7870° |
| perigee height: | 578 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 306.4384° |
| argument of perigee: | 116.3277° |
| revolutions per day: | 14.85195828 |
| mean anomaly at epoch: | 244.3049° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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