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 53854U 26145.16451337 +.00000000 +00000-0 +37280-4 0 00000
2 53854 53.2138 301.0461 0001390 78.8034 281.3114 15.08832515 05
| Epoch (UTC): | 25 May 2026 03:56:53 |
| Eccentricity: | 0.0001390 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 301.0461° |
| argument of perigee: | 78.8034° |
| revolutions per day: | 15.08832515 |
| mean anomaly at epoch: | 281.3114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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