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 51968U 26144.96767774 +.00000000 +00000-0 -13654-4 0 00006
2 51968 53.1613 29.5165 0001361 94.4438 265.6718 15.31706480 01
| Epoch (UTC): | 24 May 2026 23:13:27 |
| Eccentricity: | 0.0001361 |
| inclination: | 53.1613° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 29.5165° |
| argument of perigee: | 94.4438° |
| revolutions per day: | 15.31706480 |
| mean anomaly at epoch: | 265.6718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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