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 47788U 26145.50063172 +.00000000 +00000-0 +11648-2 0 00001
2 47788 53.1553 220.9696 0003924 338.8717 21.2124 15.37435968 00
| Epoch (UTC): | 25 May 2026 12:00:54 |
| Eccentricity: | 0.0003924 |
| inclination: | 53.1553° |
| perigee height: | 451 km |
| apogee height: | 456 km |
| right ascension of ascending node: | 220.9696° |
| argument of perigee: | 338.8717° |
| revolutions per day: | 15.37435968 |
| mean anomaly at epoch: | 21.2124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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