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 53899U 26145.66668980 +.00000000 +00000-0 +41414-2 0 00000
2 53899 53.2167 323.9916 0000676 51.0281 250.8117 15.69971814 04
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0000676 |
| inclination: | 53.2167° |
| perigee height: | 359 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 323.9916° |
| argument of perigee: | 51.0281° |
| revolutions per day: | 15.69971814 |
| mean anomaly at epoch: | 250.8117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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