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 53895U 26145.66668980 +.00000000 +00000-0 +13153-2 0 00005
2 53895 53.2167 323.1704 0000509 72.9984 291.4298 15.68869302 02
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0000509 |
| inclination: | 53.2167° |
| perigee height: | 362 km |
| apogee height: | 362 km |
| right ascension of ascending node: | 323.1704° |
| argument of perigee: | 72.9984° |
| revolutions per day: | 15.68869302 |
| mean anomaly at epoch: | 291.4298° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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