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 26032.37969455 +.00000000 +00000-0 +36095-3 0 00002
2 40044 97.7650 185.4214 0049359 162.4709 197.8223 14.84558672 04
| Epoch (UTC): | 01 February 2026 09:06:45 |
| Eccentricity: | 0.0049359 |
| inclination: | 97.7650° |
| perigee height: | 580 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 185.4214° |
| argument of perigee: | 162.4709° |
| revolutions per day: | 14.84558672 |
| mean anomaly at epoch: | 197.8223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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