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 53995U 26145.53154480 +.00000000 +00000-0 +24907-4 0 00008
2 53995 53.2125 229.1256 0001250 91.7031 268.4104 15.08835050 07
| Epoch (UTC): | 25 May 2026 12:45:25 |
| Eccentricity: | 0.0001250 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 229.1256° |
| argument of perigee: | 91.7031° |
| revolutions per day: | 15.08835050 |
| mean anomaly at epoch: | 268.4104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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