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 40110U 26145.54471090 +.00000000 +00000-0 +87623-4 0 00007
2 40110 63.3790 78.4033 0388128 14.5747 346.6102 13.45437759 09
| Epoch (UTC): | 25 May 2026 13:04:23 |
| Eccentricity: | 0.0388128 |
| inclination: | 63.3790° |
| perigee height: | 799 km |
| apogee height: | 1379 km |
| right ascension of ascending node: | 78.4033° |
| argument of perigee: | 14.5747° |
| revolutions per day: | 13.45437759 |
| mean anomaly at epoch: | 346.6102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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