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 26145.38721010 +.00000000 +00000-0 +25358-3 0 00001
2 40044 97.7850 295.7048 0049184 151.5959 208.7953 14.85129329 04
| Epoch (UTC): | 25 May 2026 09:17:34 |
| Eccentricity: | 0.0049184 |
| inclination: | 97.7850° |
| perigee height: | 579 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 295.7048° |
| argument of perigee: | 151.5959° |
| revolutions per day: | 14.85129329 |
| mean anomaly at epoch: | 208.7953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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