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 51138U 26145.49612698 +.00000000 +00000-0 +53354-4 0 00008
2 51138 53.2123 314.3224 0001349 93.9406 266.1741 15.08837814 05
| Epoch (UTC): | 25 May 2026 11:54:25 |
| Eccentricity: | 0.0001349 |
| inclination: | 53.2123° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 314.3224° |
| argument of perigee: | 93.9406° |
| revolutions per day: | 15.08837814 |
| mean anomaly at epoch: | 266.1741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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