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 53988U 26145.41380181 +.00000000 +00000-0 +69607-4 0 00002
2 53988 53.2138 229.8081 0000982 86.6968 273.4136 15.08838990 06
| Epoch (UTC): | 25 May 2026 09:55:52 |
| Eccentricity: | 0.0000982 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 229.8081° |
| argument of perigee: | 86.6968° |
| revolutions per day: | 15.08838990 |
| mean anomaly at epoch: | 273.4136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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